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