Hey Jordan, I'm funning into this problem where at around the 57 min mark, when using the values you got from the trim settings, the plots in the log inspector aren't really "constant", as in they still oscillate a lot. I've pretty much copied your steps up until that point.
Hi could you please share how to control altitude for a similar model? My control has pitch angle is in the inner loop while the outer loop tries to control the altitude but for my aircraft model(following your steps for a 737-300) pid control cant find a suitable method method. My gain margin for altitude control goes inf or negative..any suggestions on this
Hi jordan , thanks for the beautiful model ....i tried to reciprocate a similar one including lateral control too (with the ailerons) but encounter some errors ...can you guide me jordan ...thanks in advance !!
For the PID controller, why is your input signal theta? If you're trying to control the flight path, shouldn't the input be gamma? Apologies for the naivete - this is an excellent tutorial.
Great work.... I need a state space model of aircraft but for a different set of states (Ref: Page-2: ocw.mit.edu/courses/aeronautics-and-astronautics/16-61-aerospace-dynamics-spring-2003/lecture-notes/lecture16.pdf). Is it possible to change the selected default system state (44:30). Can you point me to the material/source for how to change the state or a new video on that???
thank you Jordan
Knowledge worth spreading, thank you man!
Thank you for this..this is my topic for.minor project and I was so stuck before this
Nicely done, Jordan! Working on a hardware (Arduino) in the loop simulation project. Perfect resource.
Amazing!! Can you do a similar one for lateral control?
Men that was awesome thank you a lot, you teach me more than my actual teacher I appreciated your video
Amazing tutorial ! Hope you make more these tutorial videos!!!
Hey Jordan, I'm funning into this problem where at around the 57 min mark, when using the values you got from the trim settings, the plots in the log inspector aren't really "constant", as in they still oscillate a lot. I've pretty much copied your steps up until that point.
Thanks a lot, very comprehensive. :)
Can you recommend a book(s) or online resources that teach this workflow. Awesome videos!!
Hi could you please share how to control altitude for a similar model? My control has pitch angle is in the inner loop while the outer loop tries to control the altitude but for my aircraft model(following your steps for a 737-300) pid control cant find a suitable method method. My gain margin for altitude control goes inf or negative..any suggestions on this
Hi jordan , thanks for the beautiful model ....i tried to reciprocate a similar one including lateral control too (with the ailerons) but encounter some errors ...can you guide me jordan ...thanks in advance !!
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For the PID controller, why is your input signal theta? If you're trying to control the flight path, shouldn't the input be gamma? Apologies for the naivete - this is an excellent tutorial.
Could you please explain why we could not stable the h? It seems that h is always decrease. But if it would be a autopilot, shouldn't h be stable?
Great work.... I need a state space model of aircraft but for a different set of states (Ref: Page-2: ocw.mit.edu/courses/aeronautics-and-astronautics/16-61-aerospace-dynamics-spring-2003/lecture-notes/lecture16.pdf). Is it possible to change the selected default system state (44:30). Can you point me to the material/source for how to change the state or a new video on that???
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