Title :
Research on speediness stability of flight vehicle based on maximum principle
Author :
Yao, Jun ; Wang, Xin ; Chen, Tao ; Wang, Yuxin
Author_Institution :
Shenyang Ligong Univ., Shenyang
Abstract :
Based on modern optimization control maximum principle, the results of optimization control moment are given on the condition that the range of aircraft roll disturbance is fixed and the control is restricted. This method can conquer the disturbance of roll in the shortest time, which can ensure the stability of flight.
Keywords :
aerospace control; aircraft; optimisation; vehicle dynamics; velocity control; aircraft roll disturbance; flight stability; flight vehicle; optimization control maximum principle; optimization control moment; speediness stability; Aerospace control; Aircraft; Boundary conditions; Constraint optimization; Control theory; Differential equations; Mathematical model; Stability; TV broadcasting; Vehicle dynamics;
Conference_Titel :
Industrial Electronics and Applications, 2008. ICIEA 2008. 3rd IEEE Conference on
Conference_Location :
Singapore
Print_ISBN :
978-1-4244-1717-9
Electronic_ISBN :
978-1-4244-1718-6
DOI :
10.1109/ICIEA.2008.4582708
