Optimal control for space capture of noncooperative target

Ji Feng Guo; Li Jia Zhang; Nai Gang Cui

doi:10.3873/j.issn.1000-1328.2010.02.014

Optimal control for space capture of noncooperative target

Ji Feng Guo^*
, Li Jia Zhang
, Nai Gang Cui

^*Corresponding author for this work

School of Astronautics

Beijing Institute of Astronautical Systems Engineering

Research output: Contribution to journal › Article › peer-review

5 Scopus citations

Abstract

Fuel optimal control for capture of a free tumbling target considering collision avoidance is studied. To rescue the control-deficient target spacecraft, the chaser spacecraft are demanded to track the capture point at first. The model of the problem is founded, and the optimal control model is derived. According to the simulation results, the chaser spacecraft could track capture point safely with proper initial condition.

Original language	English
Pages (from-to)	386-390
Number of pages	5
Journal	Yuhang Xuebao/Journal of Astronautics
Volume	31
Issue number	2
DOIs	https://doi.org/10.3873/j.issn.1000-1328.2010.02.014
State	Published - Feb 2010

Keywords

Agile space servicing spacecraft
Noncooperative target
On-orbit servicing
Optimization rendezvous

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10.3873/j.issn.1000-1328.2010.02.014

Cite this

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title = "Optimal control for space capture of noncooperative target",

abstract = "Fuel optimal control for capture of a free tumbling target considering collision avoidance is studied. To rescue the control-deficient target spacecraft, the chaser spacecraft are demanded to track the capture point at first. The model of the problem is founded, and the optimal control model is derived. According to the simulation results, the chaser spacecraft could track capture point safely with proper initial condition.",

keywords = "Agile space servicing spacecraft, Noncooperative target, On-orbit servicing, Optimization rendezvous",

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AU - Guo, Ji Feng

AU - Zhang, Li Jia

AU - Cui, Nai Gang

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AB - Fuel optimal control for capture of a free tumbling target considering collision avoidance is studied. To rescue the control-deficient target spacecraft, the chaser spacecraft are demanded to track the capture point at first. The model of the problem is founded, and the optimal control model is derived. According to the simulation results, the chaser spacecraft could track capture point safely with proper initial condition.

KW - Agile space servicing spacecraft

KW - Noncooperative target

KW - On-orbit servicing

KW - Optimization rendezvous

UR - https://www.scopus.com/pages/publications/77951228247

U2 - 10.3873/j.issn.1000-1328.2010.02.014

DO - 10.3873/j.issn.1000-1328.2010.02.014

M3 - 文章

AN - SCOPUS:77951228247

SN - 1000-1328

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JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 2

ER -

Optimal control for space capture of noncooperative target

Abstract

Keywords

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