Reference-trajectory-planner-based integrated guidance and control under input saturation and impact angle constraint

被引:1
|
作者
Wang, Haibin [1 ]
Wang, Peng [2 ]
机构
[1] Harbin Univ Sci & Technol HUST, Coll Automat, Harbin, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut NUAA, Coll Automat Engn, Nanjing 211106, Peoples R China
关键词
Reference trajectory; command-filtered-based backstepping; guidance law; constrained control; MODEL-PREDICTIVE CONTROL; NONLINEAR-SYSTEMS; MISSILES; TRACKING; OBSERVER; VEHICLE;
D O I
10.1177/01423312221110045
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper investigates the integrated guidance and control (IGC) problem for intercepting maneuvering targets subject to the impact angle and input saturation. In order to elegantly implement tracking control under constraints, the whole controller includes the reference trajectory planner for generating reference trajectory, and the reference trajectory tracking controller for tracking the generated reference trajectory. The trajectory tracking controller is based on the command filter backstepping design under the time-domain separation, and the reference trajectory planner with a kind of reference model governor takes into account the available regulation ability of the trajectory tracking controller, so as to improve the adaptability of the proposed control scheme. The two cooperate with each other to improve the stability of guidance interception system and come out a more reasonable interception path. The simulation comparison results are provided to illustrate the superiority of the reference-trajectory-planner-based IGC law.
引用
收藏
页码:133 / 145
页数:13
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