Guiding one state of linear dynamical system to prescribed rms terminal accuracy in presence of injection, measurement and engine-mechanization error
An optimal discrete control strategy for interplanetary guidance.
1965-07-01
Miscellaneous
No indication
English
Guidance techniques for interplanetary travel
Engineering Index Backfile | 1959
|Discrete-Time Optimal Guidance
AIAA | 1999
|Discrete-Time Optimal Guidance
British Library Conference Proceedings | 1998
|