Reachable domain for satellite with two kinds of thrust

Author:

Xuehua Li,Xingsuo He,Qinfang Zhong,Ming Song

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference17 articles.

1. W. Robert, R.W. Farquhar, Near mission overview and trajectory design, AAS/AIAA Astrodynamics Conference, Halifax, Nova Scotia: AAS, 1995, pp. 8–14.

2. Near mission design;Dunham;Johns Hopkins APL Technical Digest,2002

3. Optimal low-thrust interception of earth-crossing asteroids;Conway;Journal of Guidance, Control and Dynamics,1997

4. Quadratic-based computation of four-impulse optimal rendezvous near circular orbit;Carter;Journal of Guidance, Control and Dynamics,2000

5. Low-thrust variable-specific-impulse transfers and guidance to unstable periodic orbits;Juan;Journal of Guidance Control and Dynamics,2005

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