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
Link To Document :
بازگشت