Onboard Iterative Algorithm of Defining the Parameters of Keplerian Orbits Based on Solving the Orbital Motion Equations in Velocity Reference Frame

Author:

Zubov N. E.,Ryabchenko V. N.,Lapin A. V.

Publisher

Allerton Press

Subject

Aerospace Engineering

Reference17 articles.

1. Mikrin, E.A. and Mikhailov, M.V., Navigatsiya kosmicheskikh apparatov po izmereniyam ot global’nykh sputnikovykn navigatsionnykh sistem (Spacecraft Navigation by Measurements of Global Satellite Navigation Systems), Moscow: Bauman MSTU, 2017.

2. Sokolov, N.L. and Zakharov, P.A., Autonomous Identification of Orbits Parameters of Potentially Dangerous Space Objects by Onboard Facilities, Vestnik Moskovskogo Gosudarstvennogo Universiteta Lesa – Lesnoi Vestnik, 2016, vol. 20, issue 2, pp. 214–224.

3. Battin, R.H., Astronautical Guidance, New York: McGraw-Hill Book Company, 1964.

4. Sangra, D. and Fantino, E., Review of Lambert’s Problem, Proc. of 25th International Symposium on Space Flight Dynamics (ISSFD-2015), Munich, Germany, 2015, pp. 1–15.

5. Bando, M. and Yamakawa, H., New Lambert Algorithm Using the Hamilton–Jacobi–Bellman Equation, Journal of Guidance, Control and Dynamics, 2010, vol. 33, issue 3, pp. 1000–1008.

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