Approximate analysis for relative motion of satellite formation flying in elliptical orbits
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Publication:880947
DOI10.1007/s10569-007-9067-8zbMath1119.70018OpenAlexW1992398694MaRDI QIDQ880947
He-Xi Baoyin, Fang-Hua Jiang, Jun-Feng Li
Publication date: 21 May 2007
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10569-007-9067-8
Related Items (4)
The equations of relative motion in the orbital reference frame ⋮ Effects of interplanetary dust on the LISA drag-free constellation ⋮ Frozen-anomaly transformation for the elliptic rendezvous problem ⋮ Improved initialization conditions and single impulsive maneuvers for \(J_2\)-invariant relative orbits
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- High-order analytical solutions of Hill's equations
- Useful relative motion description method for perturbations analysis in satellite formation flying
- New form for the optimal rendezvous equations near a Keplerian orbit
- Co‐ordination and control of distributed spacecraft systems using convex optimization techniques
- Dynamical behaviors and relative trajectories of the spacecraft formation flying
- SECOND APPROXIMATION TO THE SOLUTION OF THE RENDEZVOUS EQUATIONS
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