气动舵面/RCS复合控制系统构型设计与仿真
收稿日期: 2016-04-12
修回日期: 2016-05-11
网络出版日期: 2016-06-13
Design and simulation of configurations for aerodynamic surfaces/RCS blended control system
Received date: 2016-04-12
Revised date: 2016-05-11
Online published: 2016-06-13
鹿存侃 , 胡永太 . 气动舵面/RCS复合控制系统构型设计与仿真[J]. 航空学报, 2016 , 37(S1) : 106 -111 . DOI: 10.7527/S1000-6983.2016.0167
According to the blended control problem of aerospace vehicle with multiple control effectors during the reentry phase, based on the characteristics of aerodynamic surfaces and pulsed reaction control jets, three different compound controller configurations are proposed:command configuration, moment configuration and command error configuration. The corresponding control laws are also developed to complete the control system design for the reentry phase of aerospace vehicle. Simulation results show that all of the three control systems have strong abilities of tracking command rapidly. The smoothest responding of aerodynamic surface and the least frequency firing of jets are achieved with the command configuration controller. According to the work of effectors, the command configuration controller is the most effective in practice.
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