The following paper is presented in viewgraph format and topics include: (1) exact solutions are difficult to obtain for higher order systems; (2) impulsive forces cannot be implemented directly; (3) exact solution provide the basis for judging the optimality of approximate techniques; and (4) properties of the exact solution can be used to develop improved approximations. Furthermore, the author discusses a floating harmonic oscillator whose model possesses rigid and flexible body motion characteristics of the proposed spacecraft.
Fuel Optimal Propulsive Reboost of Flexible Spacecraft
1992
15 pages
Report
No indication
English
Fuel optimal propulsive reboost of flexible spacecraft
AIAA | 1992
|Fuel-Optimal Propulsive Reboost of Flexible Spacecraft
Online Contents | 1993
|Fuel optimal propulsive reboost of flexible spacecraft
NTRS | 1992
|Fuel-optimal propulsive reboost of flexible spacecraft
AIAA | 1993
|Fuel-optimal propulsive reboost of flexible spacecraft
NTRS | 1993
|