The SAINTaholic
New Member
- Joined
- Jan 4, 2008
- Messages
- 4
We make canopys for aircraft. Some of these canopys need to have different types of coatings on their concaved surfaces. We have a robot that has the capability to do this but it needs the roll pitch and yaw values to be able to program it correctly. We do have all the "points" of the surfaces on CAD..... The idea is to be able to simply open up an Excel sheet with this formulation and type in the "ijk" values ("points" in CAD) which will pop up the Roll Pitch and Yaw values.....
Incase anybody is wondering; the formulation is:
Z″(α)oX′(β)oZ(γ) = [ (X′(β)z(γ)) o z(α) o (X′(β)z(γ))−1 ] o X′(β) o z(γ)
= [ {z(γ)x(β)z(−γ) z(γ)} o z(α) o {z(−γ) z(γ)x(−β)z(−γ)} ] o [ z(γ)x(β)z(−γ) ] o z(γ)
= z(γ)x(β)z(α)x(−β)x(β) = z(γ)x(β)z(α) .
http://en.wikipedia.org/wiki/Tait-Bryan_angles
We just dont know how to insert this formula into Excel so that all we have to do is type in the ijk unit vectors......
Thank you in advanced....
Ron
Incase anybody is wondering; the formulation is:
Z″(α)oX′(β)oZ(γ) = [ (X′(β)z(γ)) o z(α) o (X′(β)z(γ))−1 ] o X′(β) o z(γ)
= [ {z(γ)x(β)z(−γ) z(γ)} o z(α) o {z(−γ) z(γ)x(−β)z(−γ)} ] o [ z(γ)x(β)z(−γ) ] o z(γ)
= z(γ)x(β)z(α)x(−β)x(β) = z(γ)x(β)z(α) .
http://en.wikipedia.org/wiki/Tait-Bryan_angles
We just dont know how to insert this formula into Excel so that all we have to do is type in the ijk unit vectors......
Thank you in advanced....
Ron