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首页> 外文期刊>Acta astronautica >Integration planning of gimbal angle and attitude motion for zero propellant maneuver under attitude and control moment gyroscope constraints
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Integration planning of gimbal angle and attitude motion for zero propellant maneuver under attitude and control moment gyroscope constraints

机译：姿态和控制力量陀螺仪陀螺仪约束零推进机动陀螺仪陀螺仪陀螺仪的整合规划

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摘要

Zero propellant maneuver is an advanced concept of large spacecraft attitude control that has recently been applied to International Space Station. The objective of this paper is the zero propellant maneuver path planning of space station under attitude and control moment gyroscope constraints. First, a multi-constraint model of zero propellant maneuver with single gimbal control moment gyroscopes is established. Then, an integrated planning algorithm of gimbal angle and attitude motion is proposed: Local Control Differential Evolution. The algorithm can simultaneously handle attitude constraints and control moment gyroscope constraints to obtain an attitude path that satisfies the attitude constraints and a gimbal angle path that is far from singularly and saturation. In addition, the algorithm combines the local control algorithm with the global differential evolution algorithm. The local control algorithm based on the potential function idea can better deal with local attitude obstacle constraints, and the global optimization algorithm based on the improved differential evolution algorithm can perform global gimbal angle optimization. Finally, simulation results show that the method is effective in dealing with both attitude and control moment gyroscope constraints.
机译：零推进剂机动是最近应用于国际空间站的大型航天器态度控制的先进概念。本文的目的是在姿态和控制力矩陀螺仪约束下的空间站零推进剂操纵路径规划。首先，建立了单个万向节控制力矩陀螺仪的零推进剂操纵的多约束模型。然后，提出了一种万能角度和姿态运动的综合规划算法：局部控制差分演进。该算法可以同时处理姿态约束和控制力矩陀螺仪约束，以获得满足姿态约束的姿态路径和远离奇差和饱和的万向角路径。此外，该算法将局部控制算法与全局差分演进算法相结合。基于潜在功能思想的本地控制算法可以更好地处理局部姿态障碍约束，基于改进的差分演进算法的全局优化算法可以执行全局万向节角度优化。最后，仿真结果表明，该方法在处理姿态和控制力矩陀螺仪约束方面是有效的。

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  • 来源
    《Acta astronautica》 |2020年第7期|123-133|共11页
  • 作者

    Wang Zhuo; Xu Rui; Zhu Shengying; Jiang Huiping; Li Zhaoyu; Liang Zixuan; Luo Da;

  • 作者单位

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Minist Ind & Informat Technol Key Lab Autonomous Nav & Control Deep Space Explo Beijing 100081 Peoples R China;

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Minist Ind & Informat Technol Key Lab Autonomous Nav & Control Deep Space Explo Beijing 100081 Peoples R China;

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Minist Ind & Informat Technol Key Lab Autonomous Nav & Control Deep Space Explo Beijing 100081 Peoples R China;

    Minzu Univ China Sch Informat Engn Beijing 100081 Peoples R China;

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Minist Ind & Informat Technol Key Lab Autonomous Nav & Control Deep Space Explo Beijing 100081 Peoples R China;

    Beijing Inst Technol Sch Aerosp Engn Beijing 100081 Peoples R China|Minist Ind & Informat Technol Key Lab Autonomous Nav & Control Deep Space Explo Beijing 100081 Peoples R China;

    Shanghai Inst Satellite Engn Shanghai 200240 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Zero propellant maneuver; Singularity and saturation; Local control; Attitude maneuver planning;

    机译：零推进式机动;奇点和饱和;局部控制;态度操纵计划;

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