How to Estimate Microaccelerations for Spacecraft with Elliptical Orbit

Author:

Sedelnikov A. V.,Potienko K. I.

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,General Physics and Astronomy,General Engineering,Modeling and Simulation

Reference20 articles.

1. Belousov, A.I., Sedelnikov, A.V.: Problems in formation and control of a required microacceleration level at spacecraft design, tests, and operation. Russian Aeronautics 57(2), 111–117 (2014)

2. Beuselinck, T., Van Bavinchove, C., Abrashkin, V.I., Kazakova, A.E., Sazonov, V.V.: Determination of the spacecraft Foton M-3 attitude motion on measurements of the Earth magnetic field, Preprint of Keldysh Institute of Applied Mathematics Russian Academy of Sciences. 𝒩 $\mathcal {N}$ o̱ 80 (2008)

3. Bezglasnyi, S.P.: Active orientation of a gyrostat with variable moments of inertia. J. Appl. Math. Mech. 78 (6), 766–777 (2014)

4. Bojko, A.N., Zavodjan, A., Simonov, B.M.: Micromechanical accelerometers: modeling of elements of a design and production. Electronics: Science, technology, business 8, 100–103 (2009)

5. Doroshin, A.V., Neri, F.: Open research issues on nonlinear dynamics, dynamical systems and processes. WSEAS Trans. Syst. 13, 644–647 (2014)

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