Algorithm for balancing a platform on aerodynamic suspension for ground development of nanosatellite control systems

Author:

Tasheva V. I.,Kramlikh A. V.,Lomaka I. A.

Publisher

AIP Publishing

Reference18 articles.

1. The UVSQ-SAT/INSPIRESat-5 CubeSat Mission: First In-Orbit Measurements of the Earth’s Outgoing Radiation

2. A First Experience of Space Radiation Monitoring in the Multi-Satellite Experiment of Moscow University in the Framework of the Universat-SOCRAT Project

3. Gupta, M. Design of a polar elliptical orbit for a nanosatellite at LEO altitude of 475 km/725 km with maximum coverage of the world for seismic wave detection, 2020, Journal of Physics: Conference Series, 1507 (10), No. 102038.

4. Mezhankov K.V. Data collection technology on the near-Earth space and the Earth seismic activity based on the nanosatellites. Youth and Science. Thesis of reports at the XVI International telecommunications conference of young scientists and students. 2013, p. 94.

5. M.D. Koptev, N.N. Proshunin, D.S Ivanov. Determination of motion of the nanosatellite control system model on the aerodynamic table using the video camera. Preprints, Keldysh IAM, 2015, p. 109.

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