• DocumentCode
    2716379
  • Title

    Bio-inspired computing for launch vehicle design and trajectory optimization

  • Author

    Suresh, Sundaram ; Rong, Hai-Jun ; Sundararajan, Narasimhan

  • Author_Institution
    Dept. of Electr. Eng., Indian Inst. of Technol., Delhi, India
  • fYear
    2009
  • fDate
    8-10 July 2009
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    This paper presents an optimization tool for launch vehicle design and trajectory optimization using bio-inspired computing algorithms and nonlinear programming. The objective is to size a launch vehicle such that the payload to lift-of-weight ratio is maximized (i.e the lift off weight is a minimum). Here, the staging problem is solved using Particle Swarm Optimization (PSO) method. With the above vehicle, an optimal trajectory is arrived at using a Real-Coded Genetic Algorithm (RCGA) and solving a nonlinear programming (NLP) by the direct shooting method. The solutions from PSO and RCGA are used for initialization of NLP variables. A case study is carried out that establishes the advantage of the proposed approach.
  • Keywords
    aircraft; genetic algorithms; nonlinear programming; particle swarm optimisation; position control; bio-inspired computing; launch vehicle design; nonlinear programming; particle swarm optimization; real-coded genetic algorithm; trajectory optimization; Algorithm design and analysis; Design optimization; Engines; Genetic algorithms; Orbits; Particle swarm optimization; Propulsion; Rockets; Satellites; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computational Intelligence for Security and Defense Applications, 2009. CISDA 2009. IEEE Symposium on
  • Conference_Location
    Ottawa, ON
  • Print_ISBN
    978-1-4244-3763-4
  • Electronic_ISBN
    978-1-4244-3764-1
  • Type

    conf

  • DOI
    10.1109/CISDA.2009.5356548
  • Filename
    5356548