Autonomous Control Program for Special Spacecraft Debris Collector Rendezvous Transfer with Fragment of Space Debris with Low-thrust

Author:

Ishkov Sergey A.,Filippov Gregory A.,Khramov Andrew A.

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference6 articles.

1. S.A. Ishkov, G.A. Filippov, Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine, Vestnik of the Samara university, Is. 4(46), (2014), pp. 30-38.

2. S.A. Ishkov, P.V. Fadeenkov, V.L. Balakin Assessing the efficiency of flights to high near-earth orbits using boosters with chemical and electro-rocket engines, Vestnik of the Samara university, Is. 2 (33), (2012), pp. 48-55.

3. P.V. Fadeenkov, S.A. Ishkov Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits, Vestnik of the Samara university, Is. 1 (25), (2011), pp. 31-37.

4. P.V. Fadeenkov Optimization of flights between non-coplanar circular orbits with a two-stage booster with chemical and electrojet engines, Vestnik of the Samara University, Is. 1 (12), (2007), pp. 116-122.

5. S.A. Ishkov, G.A. Filippov A disposal of the space debris with special spacecraft debris collector using low thrust, Engineering Letters, Is. 23(2), (2015), pp. 98-109.

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