Prediction and Correction of Spacecraft Motion Based on the Solutions of Regular Quaternion Equations in KS-Variables and Isochronous Derivatives
Author:
Affiliation:
1. Russian Academy of Sciences Institute of Precision Mechanics and Control,Saratov,Russia
Funder
Russian Science Foundation
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9815262/9815332/09815441.pdf?arnumber=9815441
Reference21 articles.
1. Quaternion Regularization of the Equations of the Perturbed Spatial Restricted Three-Body Problem: II
2. Quaternion methods and models of regular celestial mechanics and astrodynamics
3. Design of optimum control strategies and trajectories of a Spacecraft with the regular quaternion equations of the two body problem;sapunkov;Cosmic Research,1996
4. Quaternion construction of optimum managements and trajectories of movement of a space vehicle in the newtonian gravitational field;chelnokov;Mech Solids,1996
5. Analysis of optimal motion control for a material point in a central field with application of quaternions
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