A NEW KINEMATIC METHOD FOR FLYING-AROUND SATELLITE FORMATION DESIGN

LU Hongwei; XI Xiaoning; YU Qifeng

doi:10.11728/cjss2004.02.20040207

Volume 24 Issue 2

Mar. 2004

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Article Navigation > Chinese Journal of Space Science > 2004 > 24(2): 124-131

LU Hongwei, XI Xiaoning, YU Qifeng. A NEW KINEMATIC METHOD FOR FLYING-AROUND SATELLITE FORMATION DESIGN[J]. Chinese Journal of Space Science, 2004, 24(2): 124-131. doi: 10.11728/cjss2004.02.20040207

Citation:

LU Hongwei, XI Xiaoning, YU Qifeng. A NEW KINEMATIC METHOD FOR FLYING-AROUND SATELLITE FORMATION DESIGN[J]. Chinese Journal of Space Science, 2004, 24(2): 124-131. doi: 10.11728/cjss2004.02.20040207

LU Hongwei, XI Xiaoning, YU Qifeng. A NEW KINEMATIC METHOD FOR FLYING-AROUND SATELLITE FORMATION DESIGN[J]. Chinese Journal of Space Science, 2004, 24(2): 124-131. doi: 10.11728/cjss2004.02.20040207

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A NEW KINEMATIC METHOD FOR FLYING-AROUND SATELLITE FORMATION DESIGN

doi: 10.11728/cjss2004.02.20040207 cstr: 32142.14.cjss2004.02.20040207

College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073

Received Date: 2003-06-12
Rev Recd Date: 2003-11-10

Abstract

Abstract

This paper presents a new kinematic design method for satellite formation. First, the kinematic of the relative motion of zero inclination satellite formation is analyzed and orbit design is investigated. And orbit transformation method is proposed for arbitrary inclination satellite formation orbit design. Finally, the simulation results show that the method is effective and feasible.
- Formation flying,
- Small inclination,
- Kinematics method,
- Orbit elements