Analytical Quasi-Optimal Algorithm for Program Control of an Attitude of an Axisymmetric Spacecraft
Author:
Affiliation:
1. Institute of Precision Mechanics and Control of RAS,Saratov,Russia
2. Yu.A. Gagarin Saratov State Technical University,Saratov,Russia
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10168302/10168309/10168467.pdf?arnumber=10168467
Reference5 articles.
1. Solution of Approximate Equation for Modified Rodrigues Vector and Attitude Algorithm Design
2. On oscillatory and rotational motions of the one class of mechanical systems;chelnokov;Izv AN SSSR Mekhanika Tverdogo Tela,1989
3. Analytical Quasi-Optimal Solution for the Problem on Turn Maneuver of an Arbitrary Solid with Arbitrary Doundary Conditions
4. Special control regime in the problem of optimal turn of an axially symmetric spacecraft
5. Analytical solution of the optimal slew problem for an axisymmetric spacecraft in the class of conical motions
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