Orbit determination using analytic partial derivatives of perturbed motion
- 1 January 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (1) , 4-12
- https://doi.org/10.2514/3.5597
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- An investigation into the effects of using simplified force models in the computation of state transition matricesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- The matrizant of keplerian motionAIAA Journal, 1964
- Differential Expressions for Low-Eccentricity Geocentric OrbitsPublished by Springer Nature ,1960