Optimal control for the rolling pullout maneuver of a modern fighter aircraft
| Data(s) |
02/04/2007
|
|---|---|
| Resumo |
Optimal control laws are obtained for the elevator and the ailerons for a modern fighter aircraft in a rolling pullout maneuver. The problem is solved for three flight conditions using the conjugate gradient method. |
| Formato |
application/pdf |
| Identificador |
http://eprints.iisc.ernet.in/42911/1/OPTIMAL_CONTROL.pdf Satyanarayana, G and Sarma, IG and Prasad, UR (2007) Optimal control for the rolling pullout maneuver of a modern fighter aircraft. In: 1975 IEEE Conference on Decision and Control including the 14th Symposium on Adaptive Processes, Dec. 1975. |
| Publicador |
IEEE |
| Relação |
http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumber=4045457&tag=1 http://eprints.iisc.ernet.in/42911/ |
| Palavras-Chave | #Aerospace Engineering (Formerly, Aeronautical Engineering) |
| Tipo |
Conference Paper PeerReviewed |
