• DocumentCode
    25225
  • Title

    Reachability Using Arbitrary Performance Indices

  • Author

    Holzinger, Marcus J. ; Scheeres, Daniel J. ; Hauser, John

  • Author_Institution
    Georgia Inst. of Technol., Atlanta, GA, USA
  • Volume
    60
  • Issue
    4
  • fYear
    2015
  • fDate
    Apr-15
  • Firstpage
    1099
  • Lastpage
    1103
  • Abstract
    The problem of optimal reachability set computation with alternate performance indices and independent parameters for smooth value functions is motivated and examined. A General Independent Parameter Hamilton Jacobi Bellman PDE formulation is derived and an independent parameter mapping function is defined. Performance index metric properties are leveraged to define Generalized Metric Range Sets. For Newtonian systems it is shown that singular independent parameter mappings can be circumvented using constants of motion. Finally, the motivating problem is solved using the central results of this technical note to generate free-time, Δν-constrained orbital metric range sets.
  • Keywords
    aerospace control; fuel; optimal control; partial differential equations; performance index; reachability analysis; Newtonian systems; alternate performance indices; arbitrary performance indices; fuel-optimal control; general independent parameter Hamilton Jacobi Bellman PDE formulation; generalized metric range sets; independent parameter mapping function; independent parameter mappings; motion constant; optimal reachability set computation; orbital metric range sets; performance index metric properties; smooth value functions; spacecraft; Dynamics; Fuels; Measurement; Optimal control; Optimized production technology; Space vehicles; Trajectory; Hamilton Jacobi Bellman partial differential equation (HJB PDE); Range; Reachability;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9286
  • Type

    jour

  • DOI
    10.1109/TAC.2015.2391451
  • Filename
    7014247