空间太阳能电站编队构型重构控制算法  

Control algorithm of formation configuration reconfiguration of space solar power station

作　　者：杨靖宇[1,2] 丁赟 郝运 YANG Jing-yu;DING Yun;HAO Yun(Intelligent Aircraft System Theory and Technology Laboratory,Shenyang Aerospace University,Shenyang 110136,China;Research and Development Department,Shenyang Goddard Intelligent Equipment Technology Co.Ltd.,Shenyang 110001,China;Chendu Aircraft Industry(Group)Co.Ltd.,Chengdu 610073,China)

机构地区：[1]沈阳航空航天大学智能飞行器系统理论与技术实验室,沈阳110136 [2]沈阳戈达德智能装备科技有限公司研发部,沈阳110001 [3]成都飞机工业(集团)有限责任公司,成都610073

出　　处：《沈阳航空航天大学学报》2022年第4期1-9,共9页Journal of Shenyang Aerospace University

基　　金：中国高校产学研创新基金(项目编号:2021BCF01004);中国学位与研究生教育学会面上项目(项目编号:2020MSA227)。

摘　　要：为了使空间太阳能电站编队飞行时能够进行队型重构变换,首先,基于同步根数差法推导了地球静止轨道上的空间太阳能电站编队运动型模型,设计了合适的空间太阳能电站编队构型,确保其在任意环境下都可以维持正常的能量传输。其次,基于传统的循环追踪控制算法进行编队重构的仿真,提出改进循环追踪控制算法并进行仿真验证。仿真结果表明,改进后的循环追踪控制算法可以有效地实现编队重构。In order to enable the formation reconfiguration transformation of space solar power stations in formation flight,the formation motion model of space solar power station on the geostationary orbit was deduced based on the synchronous root number difference method,and the appropriate formation configuration of space solar power station was designed to ensure that it can maintain normal energy transmission in any environment.Secondly,the simulation of formation reconfiguration was carried out in combination with the traditional loop tracking control algorithm,and an improved loop tracking control algorithm was designed,and the simulation verification was carried out.The simulation results show that the improved loop tracking control algorithm can effectively realize formation reconfiguration.

关 键 词：空间太阳能电站 编队飞行 同步根数差法 编队重构 循环追踪控制算法 

分 类 号：V47[航空宇航科学与技术—飞行器设计]