Optimal Release Control of Companion Satellite System Using Electromagnetic Forces
Zengwen Xu, Peng Shi,Yushan Zhao
(School of Astronautics, Beihang University, Beijing 100191, China)
Abstract:
Electromagnetic forces generated by the inter-action of component satellites can be used to release companion satellites. Optimal release trajectories for companion satellite system using inter-electromagnetic forces were investigated. Firstly, nonlinear relative motion dynamic equations of a two-craft electromagnetic companion satellite system were derived in spatial polar coordinates. Then principles of electromagnetic satellite formation flying were introduced. Secondly, the characteristics of the electromagnetic companion satellites release were analyzed and optimal release trajectories of companion satellites using electromagnetic forces were obtained using Gauss pseudospectral method. Three performance criteria were chosen as minimum time, minimum acceleration of the separation distance and minimum control acceleration. Finally, three release examples including expansion along separation distance, rotation in orbital plane and stable formation reconfiguration were given to demonstrate the feasibility of this method. Results indicated that the release trajectories can converge to optimal solutions effectively and the concept of release companion satellites using electromagnetic forces is practicable.
Key words: companion satellites electromagnetic formation flying optimal release trajectory Gauss pseudospectral method
DOI：10.11916/j.issn.1005-9113.2015.04.004
Clc Number:V412.4
Fund:
删除或更新信息，请邮件至freekaoyan#163.com(#换成@)
Optimal Release Control of Companion Satellite System Using Electromagnetic Forces
本站小编 哈尔滨工业大学/2019-10-23
相关话题/Optimal Release Control Companion Satellite
领限时大额优惠券,享本站正版考研考试资料!
优惠券领取后72小时内有效，10万种最新考研考试考证类电子打印资料任你选。涵盖全国500余所院校考研专业课、200多种职业资格考试、1100多种经典教材，产品类型包含电子书、题库、全套资料以及视频，无论您是考研复习、考证刷题，还是考前冲刺等，不同类型的产品可满足您学习上的不同需求。 ...考试优惠券 本站小编 Free壹佰分学习网 2022-09-19GEO Satellite Thruster Configuration and Optimization
GEO Satellite Thruster Configuration and Optimization Author NameAffiliationJiajia FengBeijing Institute of Control Engineering, Beijing 100190, ChinaScience and Technology on Space Intelligent Control Laboratory,Beijing 100190,ChinaZuowei WangBeijing Institute of Control En ...哈尔滨工业大学科研学术 本站小编 哈尔滨工业大学 2020-12-05Adaptive Sliding Mode Control for the Excavator Manipulator
Adaptive Sliding Mode Control for the Excavator Manipulator Author NameAffiliationGuosheng XuSchool of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, ChinaGuangming LvSchool of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, ...哈尔滨工业大学科研学术 本站小编 哈尔滨工业大学 2020-12-05Controlled Movements in Superlubric MEMS
Controlled Movements in Superlubric MEMS Author NameAffiliationCangyu QuInstitute of Superlubricity Technology, Research Institute of Tsinghua University in Shenzhen, Shenzhen 518057, Guangdong,ChinaXiaojian XiangInstitute of Superlubricity Technology, Research Institute of ...哈尔滨工业大学科研学术 本站小编 哈尔滨工业大学 2020-12-05Review: Layer-Number Controllable Preparation of High-Quality Graphene for Wide Applications
Review: Layer-Number Controllable Preparation of High-Quality Graphene for Wide Applications Author NameAffiliationYun-Bin XieState Key Laboratory of Pollution Control and Resource Reuse, and Shanghai Institute of Pollution Control and Ecological Security, College of Environ ...哈尔滨工业大学科研学术 本站小编 哈尔滨工业大学 2020-12-05Optimal Micro-Task Scheduling for Multi-Hop D2D-Enabled Mobile Edge Computing
Optimal Micro-Task Scheduling for Multi-Hop D2D-Enabled Mobile Edge Computing Author NameAffiliationLin GaoSchool of Electronics and Information Engineering, Harbin Institute of Technology, Shenzhen 518055, Guangdong, ChinaQinyu ZhangSchool of Electronics and Information Eng ...哈尔滨工业大学科研学术 本站小编 哈尔滨工业大学 2020-12-05Novel Logarithmic Non-Singular Terminal Sliding Mode and Its Application in Attitude Control of QTR
Novel Logarithmic Non-Singular Terminal Sliding Mode and Its Application in Attitude Control of QTR Author NameAffiliationHaibo LiuCollege of Aeronautics，Northwestern Polytechnical University， Xi’an 710072, ChinaHeping WangCollege of Aeronautics，Northwestern Polytechnical Un ...哈尔滨工业大学科研学术 本站小编 哈尔滨工业大学 2020-03-06Complementary Sliding Mode Speed Control with Saturation Function Boundary Layer Optimization
Complementary Sliding Mode Speed Control with Saturation Function Boundary Layer Optimization Author NameAffiliationYanwei HuangCollege of Electrical Engineering and Automation, Fuzhou University, Fuzhou 350116, ChinaYuqing XieCollege of Electrical Engineering and Automation ...哈尔滨工业大学科研学术 本站小编 哈尔滨工业大学 2020-03-06Study on Thermal Deformation Measurement of Optical Remote Sensing Satellite Platform Based on Machi
Study on Thermal Deformation Measurement of Optical Remote Sensing Satellite Platform Based on Machine Vision Author NameAffiliationJie HuangShanghai Institute of Satellite Engineering, Shanghai 201109, ChinaChaolan YouShanghai Institute of Satellite Engineering, Shanghai 20 ...哈尔滨工业大学科研学术 本站小编 哈尔滨工业大学 2020-03-06An Improved Dynamic Friction Rejection Attitude Stability Control Strategy
An Improved Dynamic Friction Rejection Attitude Stability Control Strategy Author NameAffiliationYonghai WangBeijing Institute of Space Long March Vehicle, China Academy of Launch Vehicle Technology , Beijing 100076, ChinaGang MengBeijing Institute of Space Long March Vehicl ...哈尔滨工业大学科研学术 本站小编 哈尔滨工业大学 2020-03-06Design of Near-optimal Earth Escape Orbits for Solar Sail Spacecraft
Design of Near-optimal Earth Escape Orbits for Solar Sail Spacecraft Xiao-Ning Shi, Li-Tao Li, Nai-Gang Cui Dept. Astronautical Engineering, Harbin Institute of Technology, Harbin 150001,China ...哈尔滨工业大学科研学术 本站小编 哈尔滨工业大学 2019-10-24
