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A capture method of orbital net-capture system based on cooperative formation flying control

  • Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

To cope with the space debris removal mission, a capture method based on spacecraft formation flying is investigated for the orbital net-capture system. Firstly, the relative orbit motion dynamics for each payload are modeled in the local-vertical and local-horizontal rotating frame. Secondly, the flying capture trajectory for each payload is planned by the four-order polynomial. Then, a cooperative saturated PD control algorithm with computed feedforward is proposed such that all payloads can track the planned flying trajectories. This realizes the closed-loop orbital net-capture process. Finally, the simulation example of four payloads installed at the net capturing one static space debris illustrates the effectiveness of the proposed capture method.

Original languageEnglish
Title of host publicationSpaceflight Mechanics 2017
EditorsJon A. Sims, Frederick A. Leve, Jay W. McMahon, Yanping Guo
PublisherUnivelt Inc.
Pages3553-3561
Number of pages9
ISBN (Print)9780877036371
StatePublished - 2017
Event27th AAS/AIAA Space Flight Mechanics Meeting, 2017 - San Antonio, United States
Duration: 5 Feb 20179 Feb 2017

Publication series

NameAdvances in the Astronautical Sciences
Volume160
ISSN (Print)0065-3438

Conference

Conference27th AAS/AIAA Space Flight Mechanics Meeting, 2017
Country/TerritoryUnited States
CitySan Antonio
Period5/02/179/02/17

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