Journal of System Simulation
Abstract
Abstract: In this paper, a control method of satellite formation keeping is investigated based on artificial potential field. Since the N-body problem doesn’t have analytical solutions, a leader-follower formation is proposed as a restricted N-body problem. The stable structure has infinite possible pairs of coordinates in the inertial frame, therefore the Jacobian matrix of the corresponding error dynamic system at the equilibrium point is unsolvable. By introducing a transformation of coordinates from inertial frame to a specific reference frame, the stability analysis of error dynamic system is only related to the structure of formation. By the reduction of error dynamic system in the reference frame and the solving of eigenvalues of Jacobian matrix at equilibrium point, the stability analysis of the novel control method is given.
Recommended Citation
Yang, Shengqing; Ye, Wenyu; He, Yubin; and Wan, Yabin
(2019)
"Satellite Formation Keeping and Its Stability Analysis Based on Artificial Potential Field Method,"
Journal of System Simulation: Vol. 31:
Iss.
2, Article 20.
DOI: 10.16182/j.issn1004731x.joss.17-0096
Available at:
https://dc-china-simulation.researchcommons.org/journal/vol31/iss2/20
First Page
332
Revised Date
2017-04-17
DOI Link
https://doi.org/10.16182/j.issn1004731x.joss.17-0096
Last Page
339
CLC
V412.4+1
Recommended Citation
Yang Shengqing, Ye Wenyu, He Yubin, Wan Yabin. Satellite Formation Keeping and Its Stability Analysis Based on Artificial Potential Field Method[J]. Journal of System Simulation, 2019, 31(2): 332-339.
DOI
10.16182/j.issn1004731x.joss.17-0096
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