Iterative solution of least squares programming problem for finite thrust rocket trajectory optimization
Applications of a mathematical programming technique to finite thrust rocket trajectory optimization
ASTRODYNAMICS SPECIALISTS CONFERENCE ; 1971 ; FT. LAUDERDALE, FL, US
01.08.1971
Aufsatz (Konferenz)
Keine Angabe
Englisch
Trajectory of rocket with thrust
Engineering Index Backfile | 1958
|Nuclear rocket thrust optimization using dynamic programming
Engineering Index Backfile | 1963
|Approximate finite-thrust trajectory optimization.
AIAA | 1969
|