Nonlinear dynamic modeling of spacecraft relative motion in elliptical orbit via power series approach for rendezvous and proximity operations-Reference-Cited by-同舟云学术

Nonlinear dynamic modeling of spacecraft relative motion in elliptical orbit via power series approach for rendezvous and proximity operations

Published:2021-09-30 Issue:4 Volume:4 Page:281-300
ISSN:2523-3947
Container-title:Aerospace Systems
language:en
Short-container-title:AS

Author:

Ogundele Ayansola D.^ORCID,Agboola Olufemi A.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Computers in Earth Sciences,Mechanical Engineering,Social Sciences (miscellaneous),Aerospace Engineering,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42401-021-00103-z.pdf

Reference44 articles.

1. De Vries JP (1963) Elliptic elements in terms of small increments of position and velocity components. Am Inst Aeronaut Astronaut J 1(11):2626–2629

2. Alfriend K, Vadali SR, Gurfil P, How J, Breger L (2009) Spacecraft formation flying: dynamics, control and navigation, 1st edn. Butterworth-Heinemann, Oxford

3. Schaub H, Junkins JL (2014) Analytical mechanics of space systems. AIAA, New York

4. Ogundele AD, Sinclair AJ, Sinha SC (2021) Closed form parametric solutions of nonlinear abel-type and riccati-type spacecraft relative motion. Acta Astronaut 178:733–742. https://doi.org/10.1016/j.actaastro.2020.10.009

5. Ogundele AD (2021) Harmonic balance analysis and simulations of spacecraft rendezvous and formation flying dynamics. Aerospace Syst (AS). https://doi.org/10.1007/s42401-021-00083-0

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