A Mathematical Perspective on Flight Dynamics and Control (SpringerBriefs in Applied Sciences and Technology) Book Price in India, Specifications, Reviews & Offers. Buy online at Amazon.

Sir u are best ,Thanks a lot.
i think there are errors in your video in the letters used. Gamma is written in the Yaw matrix instead of Psy. Also, Psy is used instead of Phi when you calculate the changes of angles, but p is dPhi/dt, not dPsy/dt. You got me confused!
Thanks so much you have great videos!
At 3:48 the skew symmetric matrix is wrong. It should be: skew = [0 -r q; r 0 -p; -q p 0]. You did put the right one in the moment section
So in 2D, would we neglect the Z, psidot, and Iz portions?
Which master track in aerospace engineering do you think is more interesting according to you, GNC or Aerodynamics ? and if you specialized in one of these, are there job opportunities to work in aerospace, I'm just asking your opinion because I will have to decide between GNC , aero or Designing track and I find all of them fascinating so im a bit lost ..
Very well explained. Thank you
Thank you so much for this.
Kindly make corrections in it accordingly and I am wrong correct me too. At time 6.41 in your slide, in M equation, you wrote p.r (Ixx-Ixz) while if we multiply the above matrices it comes to be p.r(Ixx-Izz). Secondly, at time 3.52, the skew-symmetric matrix of wB/E, you wrote is different from the one you wrote at 6.26 time.
please make more videos on flight dynamics subject. Also kindly create a playlist in your youtube channel please.
Thanks sir u saved my semester u saved my life thanks alot
i learnt more from your videos than my uni lecture 👩‍🎓
Thanks
How to calculate the minimum thrust required for an aircraft to stay in level flight ?
1:26 Isn't 'M' = Yaw while 'N' = Pitch ??? Please correct me if I'm wrong.
sir cud u pls tell how to model an aircraft by using 6 dof
This is just rigid body dynamics, there's nothing specific to aircraft except the assumed symmetry in the inertia matrix.
Flight Dynamics not *Fight
Any recommended text book for flight dynamics?
The inertia value Ixz and Izx are the same? @7:18
Hi vinayak I need your help as I am doing simulation for bell nozzle for pressure based in which I stuck on pressure inlet that which pressure should consider for initial gauge pressure also in operational pressure.
thank you so much for the videos!! really helpful!! Can you also provide video about eigen form analysis and control ?? thanks again!!