• DocumentCode
    1794649
  • Title

    Longitudinal guidance and control of reentry vehicle in the approach and landing phase

  • Author

    Chirayath, Bynu Benjamin ; Bindu, G.R.

  • Author_Institution
    Coll. of Eng. Trivandrum, Thiruvananthapuram, India
  • fYear
    2014
  • fDate
    6-11 Jan. 2014
  • Firstpage
    1
  • Lastpage
    5
  • Abstract
    Approach and Landing phase is an important and critical part of Reusable Launch Vehicle (RLV) mission. The challenging task is to deliver a RLV to its landing site safely and reliably. Hence a control scheme has to be designed that accomplishes this task. In this paper a well tuned PID controller was first designed. Using the inputs and outputs of the PID controller a Fuzzy logic controller was designed. The controller tracks the guidance commands and limits the angle of attack in order to steer the vehicle along the desired trajectory. Simulations were performed in MATLAB for the RLV using the above two controllers. The simulation results demonstrates that the latter controller offers better performance.
  • Keywords
    aircraft landing guidance; control system synthesis; entry, descent and landing (spacecraft); fuzzy control; mathematics computing; space vehicles; three-term control; MATLAB; RLV mission; angle of attack; fuzzy logic controller; guidance commands; landing phase; reentry vehicle control; reentry vehicle longitudinal guidance; reusable launch vehicle mission; tuned PID controller; Acceleration; Aerodynamics; Fuzzy logic; Mathematical model; Trajectory; Vehicle dynamics; Vehicles; Approach and Landing; RLV; Reentry Fuzzy logic control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Signals Control and Computations (EPSCICON), 2014 International Conference on
  • Conference_Location
    Thrissur
  • Print_ISBN
    978-1-4799-3611-3
  • Type

    conf

  • DOI
    10.1109/EPSCICON.2014.6887480
  • Filename
    6887480