In area of rocket trajectory optimization, overriding considerations such as minimum takeoff or maximum payload, determine selection of single criterion of optimality; once criterion and purpose of optimization are settled, mathematical tools must be chosen for optimization analysis; physical means for choice or variation of rocket trajectory include optimal design and optimal control; first deals with distribution and shape of aerodynamic configuration; second with thrust direction and magnitude as well as aerodynamic forces.
Rocket trajectory optimization
Applied Mechanics Rev
Applied Mechanics Reviews ; 18 , n 5
1965
6 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Rocket trajectory optimization - 1950-1963
AIAA | 1991
|Air breathing engine/rocket trajectory optimization
NTRS | 1979
|Air Breathing Engine/Rocket Trajectory Optimization
NTIS | 1979
|Trajectory Optimization for Reusable Rocket Landing
IEEE | 2018
|Integrated Design-Trajectory Optimization for Hybrid Rocket Motors
Springer Verlag | 2012
|