Error analyses for the delivery of a spinning probe to Jupiter
- 1 May 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 8 (3) , 384-390
- https://doi.org/10.2514/3.19991
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- A parametric study of the behavior of the angular momentum vector during spin rate changes of rigid-body spacecraftJournal of Guidance, Control, and Dynamics, 1984
- Spacecraft Attitude Determination and ControlPublished by Springer Nature ,1978