On one approach to the optimization of low-thrust station keeping manoeuvres

Author:

Sukhanov A.A.,Prado A.F.B.A.

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference40 articles.

1. First and second isochronous derivatives in the two-body problem;Bakhshiyan;Cosm. Res.,1978

2. Barret, C.C., On the application of electric propulsion to satellite orbit adjustment and station keeping, AIAA-1967-719, American Inst of Aeronautics and Astronautics, Electric Propulsion And Plasmadynamics Conference, Colorado Springs, Colo., paper 67–719, Sep 11–13, 1967.

3. Interplanetary flights with constant output engines;Beletsky;Cosm. Res.,1964

4. Using sparse nonlinear programming to compute low thrust orbit transfers;Betts;J. Astron. Sci.,1993

5. Electrical propulsion for control of stationary satellites;Boucher;J. Spacecraft Rockets,1964

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