ature. By investigating the process of decay across various scales, we will formulate rules of generating decomposition as our design research area. These rules will evolve into design strategies for the creation and fabrication of a large-scale prototype. The design and fabrication process will be informed by the use of robotic fabrication techniques.
The three-week long programme is formulated as a two-phase process. During the two-week initial phase, participants benefit from the unique atmosphere and facilities of AA’s London home. The second phase, lasting for a week, shifts to AA’s woodland site in Hooke Park and revolves around the fabrication and assembly of a full-scale architectural intervention.
Prominent Features of the programme:
• Teaching team: Participants engage in an active learning environment where the large tutor to student ratio (5:1) allows for personalized tutorials and debates.
• Facilities: AA Digital Prototyping Lab (DPL) offers laser cutting, CNC milling, and 3d printing facilities. The facilities at AA Hooke Park allow for the fabrication of one-to-one scale prototypes with a 3-axis CNC router, various woodworking power tools, and robotic fabrication.
• Computational skills: The toolset of Summer DLAB includes but is not limited to Rhinoceros, Processing, Grasshopper, and various analysis tools.
• Theoretical understanding: The dissemination of fundamental design techniques and relevant critical thinking methodologies through theoretical sessions and seminars forms one of the major goals of Summer DLAB.
• Professional awareness: Participants ranging from 2nd year students to PhD candidates and full-time professionals experience a highly-focused collaborative educational model which promotes research-based design and making.
• Fabrication: According to the specific agenda of each year, a one-to-one scale prototype is fabricated and assembled by design teams.
• Lecture series: Taking advantage of its unique location, London, Summer DLAB creates a vibrant atmosphere with its intense lecture programme.
Eligibility: The workshop is open to architecture and design students and professionals worldwide.
Accreditation: Participants receive the AA Visiting School Certificate with the completion of the Programme.
Applications: The AA Visiting School requires a fee of £1964 per participant, which includes a £60 Visiting Membership fee. A deposit of £381 is required when registering with the online form. The deadline for applications is 20 July 2015. No portfolio or CV is required. Online application link:
https://www.aaschool.ac.uk/STUDY/ONLINEAPPLICATION/visitingApplication.php?schoolID=325
Return train tickets between London-Hooke Park, accommodation & food in Hooke Park, and materials from Digital Prototyping Lab (DPL) are included in the fees.
Programme Directors:
Elif Erdine (AA Summer DLAB Director): elif.erdine@aaschool.ac.uk
Alexandros Kallegias (AA Summer DLAB Director): alexandros.Kallegias@aaschool.ac.uk
…
elease, so for now I am back to the basics - using only what is built into the official release for the time being.
Perhaps as plugins are updated, the updated version/ release date/ download link can be added to this compatibility list. If someone has beaten me to this on another site; please let me know.
Plugins I intend to test would solicit compatibility advice for;
CENTIPEDE
CHAMELEON / WORKS /
DIVA
FAR CALCULATOR / WORKS /
FIREFLY / UPDATED / Firefly (1.0067) now works for 0.9.006. Download at www.fireflyexperiments.com
FLOWLINES / WORKS / native tools provided in 0.9 release
GENERATION / WORKS /
GECO / WORKS / update scheduled for 10.08.2012
GH KANGAROO / WORKS / plus more on the way! (per Daniel Piker)
GHOWL / WORKS /
GHYTHON / FIXED / Link to updated file; GhPython 0 5 1 0
GOAT
HAL / PARTIAL COMPATIBILITY / Fix should be available toward end of Aug.
HELIOTROPE \ BROKEN \
HOOPSNAKE
HORSTER / WORKS /
HUMMINGBIRD / WORKS /
LOCAL CODE / WORKS /
LUNCHBOX / WORKS / UPDATED 8.04 DOWNLOAD HERE
MATIS
MESHEDIT / WORKS / update scheduled for 10.08.2012
QUOKKA
SCARAB
SLINGSHOT \ BROKEN \
SOLARCIRCLES
SPIDERWEB / WORKS /
STARLING / WORKS / VER 0.2 AND 0.1
PANELING TOOLS / UPDATED / http://www.grasshopper3d.com/group/panelingtools/forum/topics/pt-gh-new-release-of-august-22-2012
WEAVERBIRD \ BROKEN \
…
ack to .ghx?
This is in relation to a discussion I've been having with David Rutten & Scott Davidson about GH consuming memory in a relatively large GH definition (~. I think what I've learned from this is that one should limit the size of the GH file, or put some incremental stops in the definition to limit the length of calculations that it runs at once. Is this a valid conclusion?
The GH file we're talking about is 7Mb & the Rhino file is about 120Mb, but when working w/ the GH def. I try to only keep about 2 curves turned on.
Here's a summary of the discussion:
Hi Mike,thanks for sending it over. I've been fiddling with the file for about 10 minutes and it climbed from 1.7 GB to 1.9GB, but then I've been switching previews on which means more meshes get calculated so you'd expect a higher memory consumption. It is possible we're leaking memory, but if you're working for hours on end, memory fragmentation might also explain part of the increase. Basically, memory gets fragmented just like disks get fragmented after prolonged use, difference is that memory cannot be defragmented unless you restart the application and allow it to start with a clean slate. I'll try and find any leaks we may have missed in the past.Goodwill,David
──────────── David Rutten
On 09/03/2011 06:19, Mike Calvino wrote:
Thanks very much David for the quick response. I've attached the files zipped. I can't figure out what's doing it. After working in the file for awhile, the memory usage in the Windows Task Manager climbs . . . it's gotten to 1.57+Gb before I exited GH & Rhino5Wip & let it dissipate, then restart & work for awhile before it does it again. It probably takes like 4 or 5 hours before it gets that high. That's the highest it's gotten, & that only happened while I was working in a Rhino file that had all of the elements baked into it - turned off at least, but it still climbed to 1.57+Gb. It seems to climbs when you work in the file & move around in both the GH def. & the Rhino file. Like turn on a few of the Extr components at the right end of the "StandareRibExtuder" groups, you can watch the MemUsage go up, but when you turn them off, it does not go down. - goes up fast at this point. Maybe I need to figure out how to do the definition with fewer components, I'm sure that's part of it, but I must confess, I think I'm still early on in the learning curve.I really hope that this is not operator error on my part & I do apologize up front if it is. I have done a disk cleanup, I have tried excluding .3dm & .ghx files from my NOD32 antivirus, no change. I hope you can find something.Let me know if you have any trouble with the files.See if you find anything & please let me know . . . thanks!Cheers! --Mike CalvinoCalvino Architecture Studio, inc.www.calvinodesign.com
…
This is the actual reason I'm going through all this. I want to develop an algorithm that can be applied consistently and produce good results.
Here is a a little background. I'm working on my master's thesis in structural analysis. My thesis is on seismic behaviour of a roman temple in Portugal. I will be using a method of analysis suitable for block structures called the discrete element method. I am using a commercial code called 3DEC for this.
Now in order to the analysis I need to construct a 3D block model of my structure. I received a 3D scan of the entire structure (in *.wrl) format and spent a week trying to clean it up and slice it into the blocks that make up the structure. Now I want to use the scanned geometry of the blocks and describe a simplified prism around each that will represent the block in my analysis. I've attached a file with one of the columns in the temple. I think (at least with my tests so far) that it is representative of the all the blocks I'm dealing with.
Now my criteria for creation of the blocks:
I would like the contact area between the blocks to be as close as possible to the actual drum contact area,
I would like to get the volume of the blocks to be as close as possible (secondary to the contact area) to the volume of the actual drums in order to insure that the weight distribution in the structure is as close to reality as possible,
I would like the shape of the contact area to be as close to reality as possible
I order to satisfy all these requirements, I've done the following in my grasshopper file:
I take a section at the top and bottom of each of the drum meshes. I use this to extract the contact outline at the top and bottom of the drum. This is sometimes problematic and requires me to clean up the model and remove features that interfere.
Next I take each surface and try to fit a minimum circle around it. I try to do this because in my mind this is the best possible way to find the actual centre of the drum when there is cut outs and deterioration. This works well as long as more than half of the contact surface is still in its circular shape (third block from bottom in the example file doesn't satisfy this requirement and thus causes problems).
Knowing the centre, I use an algorithm I created in VB to search for one of the flutes on the contact profile. My ideas is that if I can find one of the flutes, I can then find the others by just going around at 30 degrees (there are 12 flutes) and find the location of all the flutes. In the VB code I've tried to explain my algorithm so I won't explain it here. I also think this algorithm is needlessly complicated and stupid as I'll explain later.
Once I've got one of the flutes, I just find the intersection of a line with at every 30 degrees with the outline curve.
Having all (12) points around the perimeter, I use an loop to scale the shape around the centre of the circle I found in step 1 to get the area within a tolerance value of the actual contact area (satisfying requirement 1). I was using HoopSnake before, but it required resetting every time so I decided to write my own thing.
I then connect the points on both top and bottom to get a solid block.
Now the problems are as follows:
Sometimes the algorithm doesn't find the best location as the starting point. As I said an important thing is that the circle is tangent to the flutes and that is true only if the column profile is larger than a half-circle.
The software I use requires convex blocks. I've tried to remedy this by using convex hull component before step 5 to insure the surfaces are convex.
I'm having issues sometimes with the alignment of top and bottom points. I think I just need to implement a component that sorts the points around a single basis so that there is no twisting.
I've been experimenting with convex hull as a general approach for defining the corner points, but I'm having problem take the convex hull curve and breaking it into a 12 sided polygon, preserving as much as possible the location of the flutes and the general shape of the contact surface.
I'm really sorry about the long post and complicated question. I hope someone can give some pointers on what I could try. I understand that this is not an easy question and that it is more a question of doing something rather than asking about grasshopper itself. My goal is to have an algorithm that I can explain as a general method for others to use in the future when dealing with these structures. This is only a small minor part of my thesis (the analysis is what is important) but it is taking a lot of time to figure out.
If you have any other questions, I would be more than happy to provide a better explanation. In the file I have created a region with all my input parameters. You can choose a different mesh from that point and change various settings. I hope that is self-explanatory.
Thanks for all your help,
Ali
BTW: I'm really sorry for the poor way I've done this stuff so far. I'm not a programmer and apart from some small macros in Excel I don't know much about this stuff. To add to that, I've just started with Rhino and Grasshopper about five days ago after almost pulling out all my hair trying to do this with AutoCAD!…
lly it should not make much of a difference - random number generation is not affected, mutation also is not. crossover is a bit more tricky, I use Simulated Binary Crossover (SBX-20) which was introduced already in 1194:
Deb K., Agrawal R. B.: Simulated Binary Crossover for Continuous Search Space, inIITK/ME/SMD-94027, Convenor, Technical Reports, Indian Institue of Technology, Kanpur, India,November 1994
Abst ract. The success of binary-coded gene t ic algorithms (GA s) inproblems having discrete sear ch sp ace largely depends on the codingused to represent the prob lem variables and on the crossover ope ratorthat propagates buildin g blocks from pare nt strings to childrenst rings . In solving optimization problems having continuous searchspace, binary-co ded GAs discr et ize the search space by using a codingof the problem var iables in binary st rings. However , t he coding of realvaluedvari ables in finit e-length st rings causes a number of difficulties:inability to achieve arbit rary pr ecision in the obtained solution , fixedmapping of problem var iab les, inh eren t Hamming cliff problem associatedwit h binary coding, and processing of Holland 's schemata incont inuous search space. Although a number of real-coded GAs aredevelop ed to solve optimization problems having a cont inuous searchspace, the search powers of these crossover operators are not adequate .In t his paper , t he search power of a crossover operator is defined int erms of the probability of creating an arbitrary child solut ion froma given pair of parent solutions . Motivated by t he success of binarycodedGAs in discret e search space problems , we develop a real-codedcrossover (which we call the simulated binar y crossover , or SBX) operatorwhose search power is similar to that of the single-point crossoverused in binary-coded GAs . Simulation results on a number of realvaluedt est problems of varying difficulty and dimensionality suggestt hat the real-cod ed GAs with t he SBX operator ar e ab le to perform asgood or bet t er than binary-cod ed GAs wit h t he single-po int crossover.SBX is found to be particularly useful in problems having mult ip le optimalsolutions with a narrow global basin an d in prob lems where thelower and upper bo unds of the global optimum are not known a priori.Further , a simulation on a two-var iable blocked function showsthat the real-coded GA with SBX work s as suggested by Goldberg
and in most cases t he performance of real-coded GA with SBX is similarto that of binary GAs with a single-point crossover. Based onth ese encouraging results, this paper suggests a number of extensionsto the present study.
7. ConclusionsIn this paper, a real-coded crossover operator has been develop ed bas ed ont he search characte rist ics of a single-point crossover used in binary -codedGAs. In ord er to define the search power of a crossover operator, a spreadfactor has been introduced as the ratio of the absolute differences of thechildren points to that of the parent points. Thereaft er , the probabilityof creat ing a child point for two given parent points has been derived forthe single-point crossover. Motivat ed by the success of binary-coded GAsin problems wit h discrete sear ch space, a simul ated bin ary crossover (SBX)operator has been develop ed to solve problems having cont inuous searchspace. The SBX operator has search power similar to that of the single-po intcrossover.On a number of t est fun ctions, including De Jong's five te st fun ct ions, ithas been found that real-coded GAs with the SBX operator can overcome anumb er of difficult ies inherent with binary-coded GAs in solving cont inuoussearch space problems-Hamming cliff problem, arbitrary pr ecision problem,and fixed mapped coding problem. In the comparison of real-coded GAs wit ha SBX operator and binary-coded GAs with a single-point crossover ope rat or ,it has been observed that the performance of the former is better than thelatt er on continuous functions and the performance of the former is similarto the lat ter in solving discret e and difficult functions. In comparison withanother real-coded crossover operator (i.e. , BLX-0 .5) suggested elsewhere ,SBX performs better in difficult test functions. It has also been observedthat SBX is particularly useful in problems where the bounds of the optimum
point is not known a priori and wher e there are multi ple optima, of whichone is global.Real-coded GAs wit h t he SBX op erator have also been tried in solvinga two-variab le blocked function (the concept of blocked fun ctions was introducedin [10]). Blocked fun ct ions are difficult for real-coded GAs , becauselocal optimal points block t he progress of search to continue towards t heglobal optimal point . The simulat ion results on t he two-var iable blockedfunction have shown that in most occasions , the sea rch proceeds the way aspr edicted in [10]. Most importantly, it has been observed that the real-codedGAs wit h SBX work similar to that of t he binary-coded GAs wit h single-pointcrossover in overcoming t he barrier of the local peaks and converging to t heglobal bas in. However , it is premature to conclude whether real-coded GAswit h SBX op erator can overcome t he local barriers in higher-dimensionalblocked fun ct ions.These results are encour aging and suggest avenues for further research.Because the SBX ope rat or uses a probability distribut ion for choosing a childpo int , the real-coded GAs wit h SBX are one st ep ahead of the binary-codedGAs in te rms of ach ieving a convergence proof for GAs. With a direct probabilist ic relationship between children and parent points used in t his paper,cues from t he clas sical stochast ic optimization methods can be borrowed toachieve a convergence proof of GAs , or a much closer tie between the classicaloptimization methods and GAs is on t he horizon.
In short, according to the authors my SBX operator using real gene values is as good as older ones specially designed for discrete searches, and better in continuous searches. SBX as far as i know meanwhile is a standard general crossover operator.
But:
- there might be better ones out there i just havent seen yet. please tell me.
- besides tournament selection and mutation, crossover is just one part of the breeding pipeline. also there is the elite management for MOEA which is AT LEAST as important as the breeding itself.
- depending on the problem, there are almost always better specific ways of how to code the mutation and the crossover operators. but octopus is meant to keep it general for the moment - maybe there's a way for an interface to code those things yourself..!?
2) elite size = SPEA-2 archive size, yes. the rate depends on your convergence behaviour i would say. i usually start off with at least half the size of the population, but mostly the same size (as it is hard-coded in the new version, i just realize) is big enough.
4) the non-dominated front is always put into the archive first. if the archive size is exceeded, the least important individual (the significant strategy in SPEA-2) are truncated one by one until the size is reached. if it is smaller, the fittest dominated individuals are put into the elite. the latter happens in the beginning of the run, when the front wasn't discovered well yet.
3) yes it is. this is a custom implementation i figured out myself. however i'm close to have the HypE algorithm working in the new version, which natively has got the possibility to articulate perference relations on sets of solutions.
…
Analysis Tools (LAT). Our plugin has come a long way in the last 4 years and, while the legacy version will still include some small updates and contributions, we are confident in saying that the changes will be far fewer and the plugin more stable in the following months as we switch gears into the LAT effort. I can say personally that (save for a couple of small capabilities) I have made it through my list of critical features and I will hereafter be working on making these features cross-platform, cleanly-implemented, and well-documented in the new Ladybug Analysis Tools software package. As always, you can download the new release from Food4Rhino. Make sure to remove the older version of Ladybug and Honeybee and update your scripts.
The majority of changes with this release represent “icing on the cake” after a long, multi-year effort to connect to the major open source engines and datasets. So, without further adieu, here is the list of the new capabilities added with this release:
LADYBUG
Stereographic Sky Projections - Thanks to several code contributions from Byron Mardas, all Ladybug sky visualizations now support stereographic projections! Such projections are useful for understanding the hemispherical visualizations in a 2D format and they also make it easier to overlay different sky datasets on top of one another. Check here for an example file showing the sun path overlaid with helpful/harmful parts of the sky and see here for an example file using shading masks representing strategies (like an overhang) on top of the helpful / harmful portions of the sun path.
Wind Rose Upgrades - Devang Chauhan has added several new features to the Ladybug wind rose including both visual and numerical outputs of average wind velocity and frequency for each petal of the rose. Not only does this enhance the usefulness of the rose but it also paves the way for the use of the wind rose to set up CFD simulations once Butterfly is released in the near future. The new features of the wind rose can be seen in this hydra example file.
Complete Set of Local Thermal Discomfort Models - After the last release included components to evaluate radiant asymmetry discomfort (which can be modeled using these example files: 1, 2), today’s release completes Ladybug’s suite of local discomfort models from ASHRAE and the ISO by adding components to account for discomfort from cold draft. Specifically, two draft models have been added for different types of situations. The first is an older model published by P.O. Fanger, which was developed through experiments where subjects had cold air blown on the back of their neck (the most sensitive part of the body to draft). While this is useful for understanding a worst-case scenario, it can greatly overestimate the discomfort for cases of draft at ankle level - a more common occurrence that typically results from the tendency of cold air to sink. For this situation, a second draft discomfort model has been included, which is specifically meant to forecast ankle draft discomfort. The model is currently undergoing review for integration into ASHRAE-55 and a publication outlining the derivation of this model can be found here:
Liu, S., Schiavon, S., Kabanshi, A. and Nazaroff, W. (2016), Predicted Percentage Dissatisfied with Ankle Draft. Indoor Air. Accepted Author Manuscript. doi:10.1111/ina.12364 (http://escholarship.org/uc/item/9076254n).
Special thanks is due to Shichao Liu, Toby Cheung and Stefano Schiavon for sharing the model and the results of their study with the development team. The integration of draft models completes the full integration of ASHRAE-55 and EN-15251 with Ladybug. Now, you can rest assured that, if there is a certain thermal comfort standard that you need to fulfill for a given project, you can model it with the ‘bug!
Window-Based Draft Model - With the integration of draft models, the first question that one might ask is “how should these models be applied to typical design cases?” While the (soon-to-be-released) Butterfly plugin for OpenFOAM should open up a Pandora’s box of possible situations, this release of Ladybug includes a simplified downdraft model from cold vertical surfaces, which helps model several typical cases of draft discomfort. The model has been validated across several papers:
Heiselberg, P. (1994). Draught Risk From Cold Vertical Surfaces. Building and Environment, Vol 29, No. 3, 297-301
Manz, H. and Frank, T. (2003). Analysis of Thermal Comfort near Cold Vertical Surfaces by Means of Computational Fluid Dynamics. Indoor Built Environment. 13: 233-242
It has been built into the “Ladybug_Downdraft Velocity” component and has been included in an example file illustrating discomfort from cold windows in winter. The example is intended to show when glazing ratio and window U-Values are small enough to eliminate perimeter heating - a practice that is aesthetically unpleasing, costly to maintain and wasteful in its energy use.
Operative Temperature on the Psychrometric Chart - This is a feature that should have been added a long time ago but we are finally happy to say that the Ladybug_Psychrometric Chart can draw a comfort polygon assuming that the air temperature and radiant temperature are the same value (aka. an operative temperature psychrometric chart). This operative temperature chart is the format that is needed to use the ASHRAE-55 graphical method and is generally a better representation of the range of comfort in cases where one does not intend to hold the radiant temperature constant. This operative temperature capability is now set as the default on the component but you can, of course, still bring back the older comfort polygon by simply plugging in a value for meanRadiantTemperature_.
Contour Map Visualizations - Using the same inputs as the Ladybug_Recolor Mesh component, the new Ladybug_Contour Mesh component allows you to generate contoured color graphics from the results of any analysis. Now, you to maximize the use of your high-resolution studies with contours that highlight thresholds and gradients!
Image Texture Mapping for Colored Meshes - Antonello DiNunzio has added the very useful Ladybug_Texture Maker component, which allows you to bake Ladybug colored meshes with image texture maps (as opposed to the classic method that used colored vertices). This enables the creation of transparent Ladybug meshes, making it even easier to overlay Ladybug graphics with one another and with Rhino geometry:
This component also adds the ability to render Ladybug + Honeybee meshes with other rendering programs like V-Ray and 3ds Max. So you can produce Ladybug graphics like this!
Finally, image-mapped textures are also the format required for gaming and Virtual Reality software like Unity and Augmented Reality programs like Augment. So now you can export your Ladybug meshes all of the way to the virtual world!
Rhino Sun Component - If you have ever had to set up the sun for a rendering plugin and wished that you could just take your Ladybug sun and use that, then you are in luck! Byron Mardas has contributed a component that lets you set the Rhino sun based on your EPW location data, your north direction (if different from the Y-Axis) and any time of day that you want. Not only does this make it easier to coordinate the Rhino sun with your Ladybug visualizations, but you can also use it for real time shadow previews by setting your Rhino view to “Rendered” and scrolling through a slider.
Rendered Ladybug Animations - With both the image texture mapping and the Rhino sun components released, your first thought might be “it would be great if I could use this all in a rendered animation!” Thankfully, Ladybug has added a new component to help you here. The Ladybug_Render View component works in essentially the same way as the Capture View component, allowing you to make a series of images as you animate through a slider. The major benefit here is that it works with both Rhino Render and V-Ray so that animations like this can be produced effortlessly:
Cone of Vision Added - Antonello Di Nunzio has added a component that allows you to visualize various cones of vision in order to help inform your view studies. You can fine tune parameters to include just text-readable or full peripheral vision and use the resulting view cone to constrict the results of your “Ladybug_View Analysis” studies.
Terrain WIP Components Released as the Gismo Plugin - Our friend Djordje has released a new plugin Gismo - a plugin for GIS environmental analysis. As a result the following 5 terrain components: Horizon Angles, Flow Paths, Terrain Shading Mask, Terrain Generator 2, Terrain Analysis, have been removed from Ladybug+Honeybee's WIP section and are added to Gismo.
HONEYBEE
Search, Select, and Import the Hundreds Outputs from EnergyPlus/OpenStudio - Many of the power users in our community know that EnergyPlus is capable of writing several hundred different outputs from the simulation (well beyond what the basic Honeybee result readers can import). While Honeybee has always allowed one to request these outputs by adding them to the simulationOutputs_ of the component, there has not been an official workflow for searching through all of the possible outputs or importing their specific results… until now! We have added the "Honeybee_Read Result Dictionary" component, which allows you to parse the Result Data Dictionary (or .rrd file) that EnergyPlus outputs during every run of a given model. This allows you to see all of the outputs that are available for the model and you can even search through this list to find a particular output that you are interested in. Once you find what you are looking for, simply copy the text output from the component into a panel and and plug this into simulationOutputs_. Then you can use the "Honeybee_Read EP Custom Result" component to bring your custom results into GH after rerunning the simulation. The example file of an evaporative cooling tower shows how to use the workflow to request and import in the energy removed by the tower.
OpenStudio HVAC System Sizing Results - After the full integration of HVAC in the last release, we realized that a number of people wanted to run EnergyPlus models simply to evaluate the size of the Heating/Cooling system in the model (obtained from the EnergyPlus autosize calculation that is run at the start of every simulation). Such a sizing calculation can be a great way to quantify the anticipated savings from a given strategy (like shading) on the size/cost of the building’s HVAC system. To get the results of the sizing calculation, all that one needs to do is connect the output eioFile from the OpenStudio component to the Honeybee_Read HVAC Sizing component. The outputs will indicate the peak heating/cooling loads of each zone (in Watts) as well as the size of each piece of HVAC equipment in the model. The next time that you are on a project that is about to value-engineer out an exterior shading system, use the workflow in the following example file to show that the client will probably end up paying for it with a more expensive HVAC system: Quantifying HVAC Sizing Impact of Shade.
Improved Memory Usage When Building Large Energy Models - As we take the capabilities of Honeybee to larger and larger models, many of us have begun to run up against a particular limitation of our machines: memory. After upgrading our machines to have 32 GBs of RAM, there was only one way left to alleviate the problem: restructure some of the code. Honeybee now uses an enhanced approach that ensures all the previous iterations of Honeybee objects will be removed from the memory once there is a change. In any case, the considerations of memory are definitely something that we intend to improve with the future Honeybee[+] plugin.
Workflow to Import gbXML Files - While GrizzlyBear has been around for several years, enabling us to export Honeybee zones to gbXML, we have gone for quite some time without a workflow to import gbXML files to Honeybee. The new Honeybee_gbXML to Honeybee component addresses this and establishes an easier path to import models from Revit into honeybee. You can read more about the component in this post.
Window Frame Capabilities Added to OpenStudio - After the implementation of LBNL THERM / WINDOW capabilities in the last two releases, there was one final bridge to build in the Honeybee workflow - fully connecting LBNL WINDOW to Honeybee’s OpenStudio workflow. This release of Honeybee will now write all FrameAndDivider objects exported from LBNL WINDOW glazing systems into the energy simulation, enabling you to account for the frame’s thermal bridging effects. As long as the construction is brought in with the Honeybee_Import WINDOW IDF Report component, the frames associated with the construction will be assigned to all windows that have the construction. Finally, it is worth noting that the current Honeybee will also write all glass spectral data as well as gas (or gas mixture) materials into the simulation. This means that essentially all properties of any IDF export that one makes from LBNL WINDOW can be factored into the OpenStudio energy simulation (with the only exception being BSDF materials).
OpenStudio Daylight Sensors Added - In our previous releases of Honeybee, the only means of correctly account for daylight sensors in an energy simulation was to run an annual daylight simulation and use the resulting schedules for the lighting in the energy simulation. However, this can take a lot of time and work to set up and run, particularly if the daylight control (at the end of the day) will be driven by just one sensor per room. Now, we have added another option, which uses OpenStudio/EnergyPlus’s built-in daylight controls. You can assign just a point and an illuminance target on the “Set Zone Thresholds” component and the lighting will be automatically adjusted in the course of the simulation. It should also be noted that the addition of daylight sensors has also coincided with the addition of blind/shade control based on glare. The same sensor point for daylight can be used to drive dynamic shades in the energy simulation based on glare experienced at this point. This example file shows how to set up daylight controls on the EnergyPlus model and check the lighting power results to see the effect.
Better Defaults for Natural Ventilation - After many good people wrote to me informing me that Honeybee overestimates natural ventilation airflow and I wrote back showing the way that I intended natural ventilation to be set up with the component, it dawned on me that I had selected some poor component defaults. Accordingly, this release includes a window-based natural ventilation option on the Set EP Airflow component that corrects for some of the common issues that I have seen. Insect screens are included by default and the component runs a general check to see if wind-driven cross ventilation is possible before auto-assigning it. The component will air on the side of more-conservative, lower airflow rates unless the user overrides the defaults. Finally, it’s worth noting that all of these changes have not affected the freedom of the Custom WindAndStack option on the component. The new defaults can be viewed in this example file.
CFD Results Can be Plugged into Microclimate Maps - In preparation for the (very soon) release of the Butterfly that connects to the OpenFOAM CFD platform, we just wanted to note that all of the microclimate map recipes can now take an input of a csv file with a matrix of CFD results for wind speed. For the time being, we have used these to produce very high-accuracy, high resolution maps of outdoor comfort. There will be more to follow soon!
We should also note that, in the last release I mentioned that we would be phasing out the EnergyPlus component so that all efforts are focused on the OpenStudio component. While I reiterate that all of the features of the EnergyPlus component are available in the OpenStudio component and I encourage everyone to use the OpenStudio component in order to take advantage of its HVAC capabilities, I have come to realize that many prefer to use the EnergyPlus component out of habit and have not yet gotten the time to understand why the OpenStudio component is an improvement over the EnergyPlus component. As a result, we have decided to leave the EnergyPlus component in place for the time being so that everyone has more time to understand this. The future Ladybug Analysis Tools platform will only interact with EnergyPlus through OpenStudio and so it is recommended that everyone use these two components in the Honeybee plugin will serve as an educational resource to understand our current path moving forward with OpenStudio.
Lastly, it is with great pleasure that we welcome Devang Chauhan and Byron Mardas to the developer team! As mentioned previously Devang has contributed several updates to the Ladybug Wind Rose in addition to finding and solving a multitude of bugs in other components. Byron has contributed code that has enabled the previously-mentioned stereographic sky projections along with a better method for running the Ladybug Sky Mask. Finally, Byron has contributed the Rhino Sun component, which allows you to coordinate your Rhino renders with your Ladybug data. Welcome to the Ladybug team, gentlemen!
As always let us know your comments and suggestions. Cheers!
Ladybug Analysis Tools Development Team…
to incorporating math and geometry in computational design education, Paneling Tools
Marlo Ransdell, PhD Creative Director, at FSU , Digital Fabrication in Design Research and Education
Andy Payne, LIFT architects | Harvard GSD | FireFly
Jay H Song, Chair, Jewelry School of Design, Jewelry as Personal Expression, Extra+Ordinary@Jewelry.com
Pei- Jung (P.J.) Chen, Professor of Jewelry, SCAD
Gustavo Fontana, designer/co-founder nimbistand, Diseñar, desarrollar y comercializar productos por tu cuenta.
Joe Anand, CEO MecSoft Corporation, RhinoCAM
Julian Ossa, Chair, Industrial Design Director, Diseño – Una opción de vida a todo vapor!, UPB
Minche Mena, SHINE Architecture, Principal
J. Alstan Jakubiec, Daylighting and Environmental Performance in Architectural Design Solemma, LLC
Carlos Garnier R&D Director / Jaime Cadena – General Director, Plug Design, www.plugdesign.com.mx
Mario Nakov, www.chaosgroup.com [ V-Ray ]
Andres Gonzalez, RhinoFabStudio
Workshops:
o) Paneling Tools
o) RhinoCAM
o) Rhinology in Design, for Jewelry
o) Footwear
o) V-Ray: Jewelry Design
o) V-Ray: Architects and Industrial Designers
o) FireFly
o) J. Alstan Jakubiec, DIVA
The cost for each workshop or the Lectures is 95.0 US$
To register:
WORK-SHOPS April 2 - RHINO DAY
WORK-SHOPS April 3 - RHINO DAY
REGISTRATION RHINO DAY
NOTE: All students and faculty members that register to this event, will receive a Rhino 5 Educational License at the event.
…
h, and using the BScale and BDistance are creating havoc somehow too. I've simplified first, and used the Kangaroo Frames component along with setting internal iterations, to make MeshMachine act like a normal component, along with releasing the FixC and FixV. The FixV didn't make any sense anyway. I've also set Pull to 0 to speed it up during testing, since much less calculation is involved to just let the meshes collapse, prevented from disappearing altogether by using a mere 15 iterations.
Also, your breps are open so that allows much more chaos and then collapse, though they did manage to close themselves too at times. Here is closed breps with a full 45 iterations:
So now that it's working, lets re-Fix the curves, and the problem arises that there is an extra seam line that is getting fixed too, running along the cylinder, stopping the mesh from pulling tight under tension wherever a vertex happens to be near that line:
So lets grab only the naked edge curves instead:
And what happens if we lose the end caps, now that we don't have an extra line skewing the result?:
There is no real curvature differences since it's not a curvy brep so the Adapt at full 1 setting has little to do. Now what does the BScale and BDist do? Nothing! Why? Your scale is out of whack, 99 mm high cylinders but only a falloff maximum of about 5, so let's make the falloff be 25 instead, but I must restore the end caps or the meshes collapse away for some reason and freezes Rhino for a minute or so the first time I try it:
It's a start.
If I intersect the cylinders, nothing changes, since they are being treated as separate runs. MeshMachine outputs a sequence of two outputs though, due to Frames being set to a bare minimum of 2 needed to get it to work, so I filter out the original run, which is just the unmodified initial mesh it creates.
The lesson so far is that closed meshes are much less prone to collapse and glitches leading to screw ups.
A Boolean union of the cylinders is when it gets funner, here show with and without the fixed curves that seem to define boundaries too where really there are just polysurface edges:
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owing a tutorial is easy and adapting the idea of it again - it's not a fuss - i guess my skills are at 1 - since I can not yet stand alone! However I am very determined to nail this program to the ground and be at a 9 by Easter - of course that means a lot of work and hours testing - but I am young and ambitions!
I am a revit user and I just switched over (from the dark rigid side) to rhino because of a simple math problem which has to do with variations and combinations.
I am investigating the form factor for my thesis.
Form factor= building envelope (the area of the facade+the area of the roof+the area of the footprint)/the total area of the floors.
I have started by defining a specific set of parameters such as height, number of floors, maximum total floor area so I can compare the results.
Therefore the floating number will be the facade area - which in the end, considering the height is a constant - ends up being just the length of a certain shape - circle, square, triangle ...
I have done the calculation through excel after extracting from revit but only on simple shapes as follow(the following examples are my own analyzing work):
My problem is: I need a way to get all possible shapes that meet the criteria i put in - which at the moment will be defined by square meters of a floor- that is why galapagos comes in - I need it to make all possible combinations that can be computed that meet the criteria - so then the user(myself or who ever else want to use it) can make an informed choice. I am not looking for a square - circle, sphere or anything I can manually create by just using basic geometry, I am looking for all the possible combination that equal the same area.
(plan view)
After i can solve it for one level - i will constrain that all the levels add up have specific total area - so if a level get's bigger in size another one gets smaller. Again run it through Galapagos and get all possible outcomes (like the sections below)
I am aiming to get an outcome from which you have options to pick out of -> a design process not a specific shape.
You are thinking too complex - not that it's a bad thing - but I am looking for something more simplistic than that. I need a shape - windows and panels are for later use in my process and at this early stage completely irrelevant - and that will be another percentage math problem rather than aesthetics. I just need shapes to morph based on input parameters.
I hope this was an interesting read for you and I really appreciate your patience with me.…
t. This was a reasonably effective workflow for the purposes of solving the initial problem. (in reviewing this post, it seems a bit lengthy, but hopefully it's of use to others).
Link to Illustrator Script example:https://forums.adobe.com/thread/508138
Portion I used: This applies to entire illustrator document. I am using Illustrator CC 64 bit and this worked okay. Tested a few times and it failed once, but a restart of Illustrator fixed it.
var v_selection = app.activeDocument.pathItems;SwapFillStroke(v_selection); function SwapFillStroke(objSel) { for(k = 0; k < objSel.length; k++){ var subSel = objSel[k]; var c_fill = subSel.fillColor; var c_stroke = subSel.strokeColor; subSel.fillColor = c_stroke; if(!subSel.stroked) subSel.stroked = true; subSel.strokeColor = c_fill; }} redraw();
My goal was to export colored geometry, (analysis meshes for example), from Rhino and get it into illustrator with solid fills.
If you want to know how meshes are colored in rhino...there are many explanations here on the forum, a quick search will get you more detailed information.
Short version: export your lines from rhino to illustrator and run the script listed above to make the stroke color the fill color. (in illustrator, shift+X will swap the fill and stroke colors on individual objects, but does not work on multiple objects..hence the need for the script).
Detailed Version:
In my case, I had 2 case studies I was working with.1 - wind rose meshes generated from Ladybug/honeybee2 - A mesh terrain that was colored by pre-set slope values.
NOTE: There are a few plugins to bake objects with color. I used Human tools, (Bake Geometry and JustifiedText3D).http://www.grasshopper3d.com/group/human (lots of other great stuff in there too!)
I had two types of geometry. (2 different definitions)
1- An analysis mesh, (HoneyBee/LadyBug),
2 - Lines generated from mesh faces. (mesh terrain/slope values).
Export results as a DXF, and choose "do not explode". (these were my settings)
DXF seemed to produce the most consistent results.
(you could export/save as an AI file and just open them in illustrator, but that seemed to give inconsistent results with the script).
Open DXF in Illustrator:
Apply Script in illustrator:
In the terrain example, there are only 5 colors, so selection in illustrator, by color, is very easy. In the results from honeybee/ladybug, (or any analysis process I imagine), the default colors are created with a much wider range of values. I presume the legend is then created by an average of those values within a range. My point is that, with the analysis results, selecting objects by color in Illustrator is probably not a very effective workflow.
I only tested this on my instance of rhino and Illustrator. mileage may vary.
In summation, at this point, it seems that the best way to get colored mesh faces, into illustrator, is to export the meshes, (which really ends up being the mesh face edges...curves), and bringing them into illustrator and running a quick script to swap the colors. Once that is complete, you can then select ALL the objects, and change the stroke color/weight at once.…