An orbital design method for satellite formation flying

Haiying Cui, Junfeng Li, Yunfeng Gao · Journal of Mechanical Science and Technology · 2006

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Type: article
Published: 2006-02-01
Cited by: 2
References: 12
DOI: https://doi.org/10.1007/bf02915818
OpenAlex: https://openalex.org/W2004135417
Semantic Scholar: https://api.semanticscholar.org/CorpusID:109077616

Keywords

Satellite, Orbital elements, Frozen orbit, Initialization, Eccentricity (behavior)

References

Linear vs. Nonlinear Control Techniques For The Reconfiguration Of Satellite FormationsDavid J. Irvin — 2001
J2 Invariant Relative Orbits for Spacecraft FormationsHanspeter Schaub, Kyle T. Alfriend — 2001
Fundamentals of AstrodynamicsRoger R. Bate, Donald D. Mueller, Jerry E. White — 1971
Dynamic modeling and control of flexible space structuresJang-Soo Chae, Tae‐Won Park — 2003
State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference OrbitDong-Woo Gim, Kyle T. Alfriend — 2003
Dynamical behaviors and relative trajectories of the spacecraft formation flyingHexi Baoyin, Junfeng Li, Gao Yunfeng — 2002
Inverse analysis of ultrasonic signals of ceramics based on ultrasonic self-compensating techniqueJoon-Hyun Lee, Ansheng Cheng — 2006
Multi-satellite formation and reconfigurationW. Kang, Andrew G. Sparks, S.S. Banda — 2000
Geometry and control of satellite formationsHsi-Han Yeh, Andrew G. Sparks — 2000
Autonomous satellite formation assembly and reconfiguration with gravity fieldsElla Atkins, Y. Pennecot — 2002
Comparison of two methods in satellite formation flyingGao Yunfeng, Baoyin He-xi, Junfeng Li — 2003
THE RELATIVE TRAJECTORY DESIGN OF SATELLITE FORMATION FLYINGYunfeng Gao — 2003
Applied mathematics and mechanics1992

Cited by

Evaluation of fracture behavior of SA-516 steel welds using acoustic emission analysisEui Gyun Na, Kanji Ono, Dong Whan Lee — 2006
Transverse vibration of a uniform Euler-Bernoulli beam under varying axial force using differential transformation methodYoung-Jae Shin, Jong-Hak Yun — 2006

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