General-purpose rigid-body six-degrees-of-freedom program is used to solve wide variety of atmospheric flight mechanics and orbital transfer problems. Written for analysis of powered or unpowered vehicles operation near rotating oblate planet, typical applications include: guidance and flight-control system simulation and analysis, loads and dispersion-type analysis.
Optimizing simulated trajectories
NASA Tech Briefs ; 2 , 4
1978-03-01
Miscellaneous
No indication
English
Optimizing Simulated Trajectories Of Rigid Bodies
NTRS | 1989
|Optimization Of Simulated Trajectories
NTRS | 1989
|Optimizing Steady Turns for Gliding Trajectories
Online Contents | 2016
|Optimizing Trajectories for Suborbital Human Spaceflight
AIAA | 2007
|Optimizing Steady Turns for Gliding Trajectories
AIAA | 2016
|