TY - GEN
T1 - A pitch autopilot design for blended aero and reaction-jet air-to-air missile via piecewise sliding mode control
AU - Xin, Huo
AU - Peng, Jiping
AU - Ma, Kemao
AU - Zhang, Jinpeng
AU - Dong, Jipeng
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2017/1/20
Y1 - 2017/1/20
N2 - In this paper, the problem of blended aerodynamic and reaction-jet autopilot design for air-to-air missile with over-the-shoulder (OTS) launch capability is investigated, and a novel sliding mode control (SMC) approach with piecewise smooth sliding surface is applied to solve the problem. Considering the multi-actuator configuration of the agile missile, a four-order dynamical model is established where the reaction-jet control system (RCS) is arranged at the tail of the missile. By introducing piecewise sliding mode control (PSMC), elevator control and lateral force control are designed separately based on the idea of equivalent control and switched control. By the means of Gauss pseudospectral method (GPM), a minimum time optimal pitch command is obtained for numerical simulation. The simulation result verifies the effectiveness of PSMC for the blended control system.
AB - In this paper, the problem of blended aerodynamic and reaction-jet autopilot design for air-to-air missile with over-the-shoulder (OTS) launch capability is investigated, and a novel sliding mode control (SMC) approach with piecewise smooth sliding surface is applied to solve the problem. Considering the multi-actuator configuration of the agile missile, a four-order dynamical model is established where the reaction-jet control system (RCS) is arranged at the tail of the missile. By introducing piecewise sliding mode control (PSMC), elevator control and lateral force control are designed separately based on the idea of equivalent control and switched control. By the means of Gauss pseudospectral method (GPM), a minimum time optimal pitch command is obtained for numerical simulation. The simulation result verifies the effectiveness of PSMC for the blended control system.
UR - https://www.scopus.com/pages/publications/85015177767
U2 - 10.1109/CGNCC.2016.7829130
DO - 10.1109/CGNCC.2016.7829130
M3 - 会议稿件
AN - SCOPUS:85015177767
T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
SP - 2181
EP - 2186
BT - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Y2 - 12 August 2016 through 14 August 2016
ER -