KANG Chang-geng, LEI Cheng, LIU Zao-zhen. Design and Simulation of Controller for Hyper Velocity Kinetic Energy Missile[J]. JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2000, 9(1): 107-112.
Citation:
KANG Chang-geng, LEI Cheng, LIU Zao-zhen. Design and Simulation of Controller for Hyper Velocity Kinetic Energy Missile[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2000, 9(1): 107-112.
KANG Chang-geng, LEI Cheng, LIU Zao-zhen. Design and Simulation of Controller for Hyper Velocity Kinetic Energy Missile[J]. JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2000, 9(1): 107-112.
Citation:
KANG Chang-geng, LEI Cheng, LIU Zao-zhen. Design and Simulation of Controller for Hyper Velocity Kinetic Energy Missile[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2000, 9(1): 107-112.
The controller design and digital simulation for the hyper velocity kinetic energy missile is investigated. A mathematical model of the trajectory deviation from the line of sight was established, the guidance closed loop was compensated with a phase advance lag corrective network, a selecting algorithm of the attitude control motors used to steer the missile's attitude was presented. In the presence of a wide variety of disturbances the results of digital simulation are satisfactory to circular error probability(CEP) being less than 0 5?m. The steering scheme utilizing attitude control motors as actuators to control the attitude of the missile is feasible.