• 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