DocumentCode :
488147
Title :
Ascent Guidance Algorithm using Lidar Wind Measurements
Author :
Cramer, Evin J. ; Bradt, Jerre E. ; Hardtla, John W.
Author_Institution :
The Boeing Co., Seattle, WA
fYear :
1990
fDate :
23-25 May 1990
Firstpage :
254
Lastpage :
261
Abstract :
This paper discusses the formulation of a general nonlinear programming guidance algorithm that incorporates wind measurements in the computation of ascent guidance steering commands. A nonlinear programming (NLP) algorithm that is designed to solve a very general problem has the potential to meet the capability required to address the diversity demanded by future launch system. Using B-splines for the command functional form allows the NLP algorithm to adjust the shape of the command profile to achieve optimal performance. The algorithm flexibility is demonstrated by simulation of ascent with dynamic loading constraints through a set of random wind profiles with and without wind sensing capability.
Keywords :
Algorithm design and analysis; Costs; Extraterrestrial measurements; Iterative algorithms; Laser radar; Navigation; Payloads; Vehicle dynamics; Vehicles; Wind;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1990
Conference_Location :
San Diego, CA, USA
Type :
conf
Filename :
4790737
Link To Document :
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