CONTROL STRATEGIES FOR SPACE BOOSTERS USING AIR COLLECTION SYSTEMS

Citation
Hg. Kauffman et al., CONTROL STRATEGIES FOR SPACE BOOSTERS USING AIR COLLECTION SYSTEMS, Journal of spacecraft and rockets, 31(2), 1994, pp. 243-248
Citations number
10
Categorie Soggetti
Aerospace Engineering & Tecnology
ISSN journal
00224650
Volume
31
Issue
2
Year of publication
1994
Pages
243 - 248
Database
ISI
SICI code
0022-4650(1994)31:2<243:CSFSBU>2.0.ZU;2-K
Abstract
A simple and efficient performance analysis method is developed for ev aluating vehicle pitch and engine throttle controls to minimize booste r fuel required to rill second-stage liquid oxygen (LOX) tanks and del iver the vehicle to the staging point. An optimization methodology fin ds a throttle schedule that controls both the air-breathing engine and the LOX collection rate. The altitude-velocity profile is derived fro m a variational calculus/energy management contouring method. Automati c adaptive-gain pitch-rate and throttle controls are developed. Result s from a parametric study show that collecting on the run for an optim um schedule results in a 17% fuel savings over collection at a constan t Mach number.