Quadratically Constrained Linear-Quadratic Regulator Approach for Finite-Thrust Orbital Rendezvous
Journal of Guidance, Control, and Dynamics ; 35 , 6 ; 1787-1797
2012-11-01
Article (Journal)
Electronic Resource
English
Quadratically Constrained Linear-Quadratic Regulator Approach for Finite-Thrust Orbital Rendezvous
Online Contents | 2012
|British Library Conference Proceedings | 2012
|Optimal low-thrust orbital rendezvous
AIAA | 1976
|Finite-thrust explicit guidance law for nearly circular orbital rendezvous
Engineering Index Backfile | 1967
|