DocumentCode
2658665
Title
Optinal rocket trajectories: Singular control
Author
Beansan, Goh
Author_Institution
Dept of Math., Xidian Univ., Xian
fYear
2008
fDate
16-18 July 2008
Firstpage
479
Lastpage
484
Abstract
This is a brief review of singular optimal rocket trajectories and necessary conditions for their optimality. There are two forms of the compact Goh-Legendre-Clebsch necessary conditions for singular extremals in optimal control theory. The first is convenient to test the optimality of a singular extremal. The second compact form is very important but it seems to be unknown in the literature. When it is satisfied in the strengthened manner it provides sufficient conditions for the control variable to be computed in terms of the state and costate variables. We illustrate the usefulness of these compact forms of the Goh-Legendre-Clebsch conditions by a detailed analysis of a simple example. Singular extremals can be very important subarcs of optimal trajectories of rockets and aircraft in the atmosphere and in many other applications of optimal control in fisheries, economics and theoretical physics.
Keywords
aircraft control; position control; rockets; singular optimal control; Goh-Legendre-Clebsch necessary conditions; aircraft; optimal control theory; singular control; singular optimal rocket trajectory; sufficient conditions; Aerospace control; Aircraft; Aquaculture; Atmosphere; Mathematics; Optimal control; Physics; Rockets; Sufficient conditions; Testing; Goh-Legendre-Clebsch Condtions; Optimal Aircraft Trajectories; Optimal Control Theory; Optimal Rocket Trajectories; Singular Control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference, 2008. CCC 2008. 27th Chinese
Conference_Location
Kunming
Print_ISBN
978-7-900719-70-6
Electronic_ISBN
978-7-900719-70-6
Type
conf
DOI
10.1109/CHICC.2008.4605069
Filename
4605069
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