Title :
Optimal control for the rolling pullout maneuver of a modern fighter aircraft
Author :
Satyanarayana, G. ; Prasad, U. ; Sarma, I.G.
Author_Institution :
Indian Institute of Science, Bangalore, India
Abstract :
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.
Keywords :
Acceleration; Aerodynamics; Aerospace control; Aerospace engineering; Aircraft propulsion; Elevators; Equations; Gradient methods; Military aircraft; Optimal control;
Conference_Titel :
Decision and Control including the 14th Symposium on Adaptive Processes, 1975 IEEE Conference on
Conference_Location :
Houston, TX, USA
DOI :
10.1109/CDC.1975.270730
