• DocumentCode
    1889842
  • Title

    Simulation to support local search in trajectory optimization planning

  • Author

    Morris, Robert A. ; Venable, K. Brent ; Lindsey, James

  • Author_Institution
    Ames Res. Center, NASA, Moffett Field, CA, USA
  • fYear
    2012
  • fDate
    3-10 March 2012
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    NASA and the international community are investing in the development of a commercial transportation infrastructure that includes the increased use of rotorcraft, specifically helicopters and civil tilt rotors. However, there is significant concern over the impact of noise on the communities surrounding the transportation facilities. One way to address the rotorcraft noise problem is by exploiting powerful search techniques coming from artificial intelligence coupled with simulation and field tests to design low-noise flight profiles which can be tested in simulation or through field tests. This paper investigates the use of simulation based on predictive physical models to facilitate the search for low-noise trajectories using a class of automated search algorithms called local search. A novel feature of this approach is the ability to incorporate constraints directly into the problem formulation that addresses passenger safety and comfort.
  • Keywords
    aerospace safety; aerospace simulation; aerospace testing; helicopters; optimisation; search problems; NASA; artificial intelligence; automated search algorithm; civil tilt rotors; commercial transportation infrastructure; field tests; helicopters; local search; low-noise flight profiles; low-noise trajectories; passenger safety; predictive physical models; rotorcraft noise problem; simulation; trajectory optimization planning; transportation facilities; Atmospheric modeling; Computational modeling; Cost function; Noise; Search problems; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2012 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4577-0556-4
  • Type

    conf

  • DOI
    10.1109/AERO.2012.6187438
  • Filename
    6187438