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自主交会逼近段的模糊/PID混合控制
引用本文:李九人,唐国金,李海阳. 自主交会逼近段的模糊/PID混合控制[J]. 宇航学报, 2010, 31(3). DOI: 10.3873/j.issn.1000-1328.2010.03.025
作者姓名:李九人  唐国金  李海阳
作者单位:国防科技大学航天与材料工程学院105教研室,长沙,410073
摘    要:采用模糊/PID混合控制技术,对自主交会逼近段的轨道控制进行了研究。将逼近段轨道控制解耦为三个独立通道的控制,并分别设计了逼近段轨道控制的模糊控制器、PID控制器和模糊/PID混合控制器。在考虑导航和控制误差情况下,对模糊控制器、PID控制器和模糊/PID混合控制器的轨道控制情况进行了数值仿真,并对三种控制器的轨道稳定性和燃料消耗情况进行了比较。仿真结果表明,模糊/PID混合控制器的最后逼近相对运动轨迹比模糊控制器更稳定,同时燃料消耗更少。

关 键 词:自主交会  逼近段  模糊控制  PID控制  模糊/PID混合控制

Fuzzy/PID Hybrid Trajectory Control for Final Approach in Autonomous Rendezvous Mission
LI Jiu-ren,TANG Guo-jin,LI Hai-yang. Fuzzy/PID Hybrid Trajectory Control for Final Approach in Autonomous Rendezvous Mission[J]. Journal of Astronautics, 2010, 31(3). DOI: 10.3873/j.issn.1000-1328.2010.03.025
Authors:LI Jiu-ren  TANG Guo-jin  LI Hai-yang
Abstract:The trajectory control of final approach in autonomous rendezvous is studied based on fuzzy/PID hybrid control. The problem of final approach trajectory control is divided into three independent control channels, the fuzzy controller, PID controller and fuzzy/PID hybrid controller are designed respectively for each channel. Considering errors of navigation and control, numerical simulations are undertaken to verify the efficiency of the fuzzy controllers, the PID controller and the fuzzy/PID hybrid controller, and their performances are compared in terms of trajectory stability and propellant cost. It is shown that the fuzzy/PID hybrid controller can guarantee the more stable trajectory approaching with less propellant consumption.
Keywords:Autonomous rendezvous  Final approach  Fuzzy control  PID control  Fuzzy/PID hybrid control
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