Title :
Design of BTT control technology for cruise missile based on LQR
Author :
Wang, Minghao ; Liu, Gang ; Hou, Hongqing
Author_Institution :
Xi´´an Hongqing Res. Inst. of Hi-Tech, Xi´´an, China
Abstract :
Based on the LQR optimal control, a method for the BTT control of cruise missile was proposed. The mathematical model of the cruise missile based on the aerodynamic externality and aero characteristic was established. Then choose the appropriate state variable follow the design request of the control. Design the optimal control law based on the integral LQR. The simulation results show that the missile can track the command of the acceleration and roll without error, and also restrain the appearance of the sideslip.
Keywords :
aerospace control; mathematical analysis; military systems; missile control; optimal control; BTT control technology; LQR; aero characteristic; aerodynamic externality; cruise missile; mathematical model; optimal control law; Aerodynamics; Atmospheric modeling; Couplings; Elevators; Mathematical model; Missiles; Simulation; BTT control; Cruise missile; LQR;
Conference_Titel :
Artificial Intelligence, Management Science and Electronic Commerce (AIMSEC), 2011 2nd International Conference on
Conference_Location :
Deng Leng
Print_ISBN :
978-1-4577-0535-9
DOI :
10.1109/AIMSEC.2011.6009996
