Patricio Vela: Course Wiki

User Tools

Site Tools

Trace:
ece6554:project_ductedfan

Differences

This shows you the differences between two versions of the page.

Link to this comparison view

Both sides previous revisionPrevious revision
Next revision		Previous revision
ece6554:project_ductedfan [2023/03/13 11:18] – [Step 2: Nonlinear Controller] classesece6554:project_ductedfan [2024/08/20 21:38] (current) – external edit 127.0.0.1
Line 51: Line 51:
 The thrust vector angle range should be $\psi \in [-\pi/3, \pi/3]$. Make sure to implement these limits in the simulation.  It is best to design trajectories that do not hit these limits in the closed-loop. More aggressive trajectories is best saved for future self-study. The thrust vector angle range should be $\psi \in [-\pi/3, \pi/3]$. Make sure to implement these limits in the simulation.  It is best to design trajectories that do not hit these limits in the closed-loop. More aggressive trajectories is best saved for future self-study.
  
 +===== Implementation =====
 +
 +Functional code stubs for the implementation are provided in the {{ ECE6554:projects:ductedfan.zip | ducted fan zipfile}}.  They implement a constant control signal that most definitely fails to do the job, but provide enough structure to complete the project.  Comments in the code should help to realize the necessary improvements.
 ====== Activities ======= ====== Activities =======
 ----------------------- -----------------------
ece6554/project_ductedfan.1678720706.txt.gz · Last modified: 2024/08/20 21:38 (external edit)