lC_UtilEigenSystemSym (level 1) { Exception has been thrown by the target of an invocation. TargetInvocationException }
Object: MillC_UtilEigenSystemSym (level 2) { Could not load file or assembly 'Sawapansolversnet, Version=1.0.4490.29339, Culture=neutral, PublicKeyToken=null' or one of its dependencies. The system cannot find the file specified. FileNotFoundException }
Object: MillC_Topostruct2D (level 1) { Exception has been thrown by the target of an invocation. TargetInvocationException }
Object: MillC_Topostruct2D (level 2) { Could not load file or assembly 'Sawapansolversnet, Version=1.0.4490.29339, Culture=neutral, PublicKeyToken=null' or one of its dependencies. The system cannot find the file specified. FileNotFoundException }
Object: MillC_Topostruct3D (level 1) { Exception has been thrown by the target of an invocation. TargetInvocationException }
Object: MillC_Topostruct3D (level 2) { Could not load file or assembly 'Sawapansolversnet, Version=1.0.4490.29339, Culture=neutral, PublicKeyToken=null' or one of its dependencies. The system cannot find the file specified. FileNotFoundException }
Object: MillC_FEASystem (level 1) { Exception has been thrown by the target of an invocation. TargetInvocationException }
Object: MillC_FEASystem (level 2) { Could not load file or assembly 'Sawapansolversnet, Version=1.0.4490.29339, Culture=neutral, PublicKeyToken=null' or one of its dependencies. The system cannot find the file specified. FileNotFoundException }
Object: MillC_UtilFFT1D (level 1) { Exception has been thrown by the target of an invocation. TargetInvocationException }
Object: MillC_UtilFFT1D (level 2) { Could not load file or assembly 'Sawapansolversnet, Version=1.0.4490.29339, Culture=neutral, PublicKeyToken=null' or one of its dependencies. The system cannot find the file specified. FileNotFoundException }
Object: MillC_UtilFFT2D (level 1) { Exception has been thrown by the target of an invocation. TargetInvocationException }
Object: MillC_UtilFFT2D (level 2) { Could not load file or assembly 'Sawapansolversnet, Version=1.0.4490.29339, Culture=neutral, PublicKeyToken=null' or one of its dependencies. The system cannot find the file specified. FileNotFoundException }
EDIT: Even with COFF disabled in GrasshopperDeveloperSettings this still happens (Thanks Jon)
Is millipede not compatible with Rhino version 5? Or is there a different .dll to use?
Having loaded some of the components:
I congratulate you on following Rutten's 3rd law of Grasshopper :)
Although I hope the Solver and especially the Stress lines get further refinement in order to differentiate them as I find it hard to read the small label at the bottom. Maybe the Chimney's can have different numbers 3 = 3D, 2 = 2D etc.
…
t. So here we go!
1. Honeybee is brown and not yellow [stupid!]...
As you probably remember Honeybee logo was initially yellow because of my ignorance about Honeybees. With the help of our Honeybee expert, Michalina, now the color is corrected. I promised her to update everyone about this. Below are photos of her working on the honeybee logo and the results of her study.
If you think I'm exaggerating by calling her a honeybee expert you better watch this video:
Thank you Michalina for the great work! :). I corrected the colors. No yellow anymore. The only yellow arrows represent sun rays and not the honeybee!
2. Yellow or brown, W[here]TH Honeybee is?
I know. It has been a long time after I posted the initial video and it is not fun at all to wait for a long time. Here is the good news. If you are following the Facebook page you probably now that the Daylighting components are almost ready.
Couple of friends from Grasshopper community and RADIANCE community has been helping me with testing/debugging the components. I still think/hope to release the daylighting components at some point in January before Ladybug gets one year old.
There have been multiple changes. I finally feel that the current version of Honeybee is simple enough for non-expert users to start running initial studies and flexible enough for advanced users to run advanced studies. I will post a video soon and walk you through different components.
I think I still need more time to modify the energy simulation components so they are not going to be part of the next release. Unfortunately, there are so many ways to set up and run a wrong energy simulation and I really don’t want to add one new GIGO app to the world of simulation. We already have enough of that. Moreover I’m still not quite happy with the workflow. Please bear with me for few more months and then we can all celebrate!
I recently tested the idea of connecting Grasshopper to OpenStudio by using OpenStudio API successfully. If nothing else, I really want to release the EnergyPlus components so I can concentrate on Grasshopper > OpenStudio development which I personally think is the best approach.
3. What about wind analysis?
I have been asked multiple times that if Ladybug will have a component for wind study. The short answer is YES! I have been working with EFRI-PULSE project during the last year to develop a free and open source web-based CFD simulation platform for outdoor analysis.
We had a very good progress so far and our rockstar Stefan recently presented the results of the work at the American Physical Society’s 66th annual DFD meeting and the results looks pretty convincing in comparison to measured data. Here is an image from the presentation. All the credits go to Stefan Gracik and EFRI-PULSE project.
The project will go live at some point next year and after that I will release the Butterfly which will let you prepare the model for the CFD simulation and send it to EFRI-PULSE project. I haven’t tried to run the simulations locally yet but I’m considering that as a further development. Here is how the component and the logo looks like right now.
4. Teaching resources
It has been almost 11 months from the first public release of Ladybug. I know that I didn't do a good job in providing enough tutorials/teaching materials and I know that I won’t be able to put something comprehensive together soon.
Fortunately, ladybug has been flying in multiple schools during the last year. Several design, engineering and consultant firms are using it and it has been thought in several workshops. As I checked with multiple of you, almost everyone told me that they will be happy to share their teaching materials; hence I started the teaching resources page. Please share your materials on the page. They can be in any format and any language. Thanks in advance!
I hope you enjoyed/are enjoying/will enjoy the longest night of the year. Happy Yalda!
Cheers,
-Mostapha
…
erning how to do that on a sphere.
So I know already all the different approches of how to get a relaxed voronoi pattern on a free-form open surface, but still don't know how to obtain the same elegant effect on a sphere (or an ellipsoid closed surface, whatever), or how to relax the facet dome cells.
Andrew stated on his site that he used kangaroo for this project, so the Spore Lamp consists in my opinion either of a relaxed voronoi 3d diagram (b-rep, b-rep intersection) on a sphere the cells of which have been planarized later on, or more likely it is a sort of relaxed facet dome.
The trick is to:
1. obtain a nicely-balanced voronoish diagram (or facet dome cells) on a sphere
2. keep each cell/polyline planar (or force them with kangaroo to be planar) in order to move scale and loft them later on.
Here is what I have by now.(files: matsys spore lamp attempt)
That's the closest appearance that I got so far (simple move scale and loft of facet dome cells with the amount of transformations being proportional to the power of the initial cell area: bigger cell = bigger opening etc.) - with no relaxation of the diagram. But it's obviously not the same thing as the matsys design.
Here are some of my attempts of facet dome relaxation, but well, it's certainly still not the right approach, and most importantly I don't know how to keep or force the cells to be planar after the relaxation.
1. pulling vertices to a sphere - no anchor points. That obviously doesn't make sense at all, but the relaxation without anchor points gives at the beginning a pattern that is closer to what I am looking for. (files: relaxation 01)
2. pulling vertices to a sphere - two faces of the initial facet dome anchored (files: relaxation 02)
3. pulling vertices to the initial geometry (facet dome) no anchor points (files: relaxation 03)
The cell pattern of the lamp kinda looks like this:
You can find it here: http://www.grasshopper3d.com/forum/topics/kangaroo-0-095-releasedgroupUrl=kangaroo&x=1&groupId=2985220%3AGroup%3A120977&id=2985220%3ATopic%3A972434&page=2#comments
Done with Plankton (of course without the "gradient increase" appearance), but in fact not, I took a look at Daniel Parker's Plankton example files, and it's not quite the same thing. Also the cells aren't planar...
The last problem is that during the relaxation attempts that I did, the biggest initial cells became enormous, and it's not like that in the elegant project by Andrew Kudless, that I'd like to achieve.
So to sum up:
Goal no 1: Obtain an elegant voronoi /facet dome cell pattern on a sphere (or an ellipsoid surface, whatever).
Goal no 2: How to keep the cells planar in order to be able to loft them later, obtain those pyramidal forms, and assemble easily
Have you got any ideas? Or maybe there's a completely different approach to that?
Cheers, and thanks in advance…
ved in a later call to SolveInstance. Whilst the code previously worked in previous versions, I seem to be getting a component exception thrown: "parent doesn't have a valid document". It still goes on to remove the component, so I know I'm getting the canvas correctly and my component is being picked up.
Here's what happens:
I suspect the latest release must 'do' something to the document objects after SolveInstance has finished doing its business, but I'm not quite sure what and I've spent most of today struggling to resolve it.
Here is a code snippet from the class:
private GH_Component myComponent; protected override void SolveInstance(IGH_DataAccess DA) { // Get data bool token = false; DA.GetData(0, ref token); // Make a new component instance if (!token) { // Get a 'construct point' component from its guid myComponent = (GH_Component)Instances.ComponentServer.EmitObject(new Guid("3581f42a-9592-4549-bd6b-1c0fc39d067b")); // Add the component to the canvas OnPingDocument().AddObject(myComponent, false); myComponent.Attributes.Pivot = new PointF(200, 200); } // Delete the stored component else { OnPingDocument().RemoveObject(myComponent, false); return;
}
}
I wonder if anyone is having the same problem, although I suspect this may a question for you David - sorry!
Find attached.
Many thanks,
John.…
er). With the command "End Bulge" I noticed that G2 moves perpendicular to G1! But with an increase which is not equal... and is different, every time, depending on the angle between G0 and G1 and G2. How do I predict the position of G2 compared to G1 simulating the "End Bulge" command? Thank you for your professional answers.
^___^
Below you can see an example with a curve crimson ... If I move G1 of 1 unit G2 moves of 0.42 units (perpendicular) .. If I move of 2 units the next step is 0.46 unit... 3 units --> step 0,50 units... etc.
And each time changes depending on the initial conditions (G0/G1/G2 angle).
…
Added by Lucius Santo at 4:21pm on September 20, 2012
of pitch forwards and backwards2. What effect do the following have on the system... a) Angle of Attack (AOA) of the front wing b) AOA of the rear wing c) Position of the mast along the fuselage. d) Position of rider above the mast (distribution of weight between front and rear feet amd position of the mast between the feet).So, in essence I want to model a 2 dimensional system as follows...I would like to incorporate a coefficient of lift versus AOA for the front and rear wings.Data for this can be found in text file format for example here for the Eppler 817 airfoil that I want to use... EPPLER817 DATAI might need more info than this though???Assume constant velocity???Ultimately, the lift generated by the hydrofoil will equal the weight of the rider otherwise you would sink or jump forever upwards but the hydrofoil can generate more lift or less lift than the rider depending on its angle of attack. I could assume the wing can generate -1.0x to 1.5x the weight of the rider in lift?The rear wing is usually approx 1/3 the size of the front wing. So perhaps assume 1/3 of the lift of the front wing although I will probably use a different airfoil section which will have different lift characteristics.Assume the rider can shift weight forwards and backwards between front foot and rear foot to keep the foil level, but perhaps include a time lag or some means of indicating how stable the system is.Ignore the water surface and assume the wings remain submerged.I want to assess the difference between having an AOA on the front wing and no AOA on the rear wing versus no AOA on the front but a AOA that creates a downforce on the rear wing (Which is how they are normally configured I think). I believe the rear wing is alwasy trying to pitch the front wing upwards creating a greater AOA and hence more lift. The rider has to keep pressure on their front foot to stop the front wing stalling and control the lift to be equal to their weight.My aim is to understand what parameters to use for front wing AOA, rear wing AOA and mast position to create a hydrofoil that is stable but not so stable that it takes a lot of effort to pitch it forwards and backwards. So I'm not looking for the most stable configuration, I'm looking to avoid something that is really unstable or requires (for example) the rider to put 100% of weight on one foot!Is it possible to create a meaningful simulation of this with Kangaroo 1 or 2? I made a start... Not sure I've approached it in the right way and haven't attempted to add the coefficient of lift vs AOA feedback.A video of kite hydrofoiling...
More info for those still reading...Kite hydrofoils come in many shapes and sizes... there are high aspect ration wings for racing, low aspect wings for beginners / low speed. There seem to be many configurations of mast position, feet position over the mast, length of fuselage, size of front wing to rear wing etc etc. I'm planning on CNC machining the front wing, fuselage and rear wing in one piece made up from bamboo. Then applying glass fibre or carbon fibre. I already have an aluminium mast and will make a board.…
Added by martyn hogg at 1:52pm on November 14, 2016