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Information Journal Paper

Title

DESIGN OF A REACTION JET CONTROL SYSTEM FOR A VERTICAL LAUNCH FLYING VEHICLE

Pages

  59-70

Abstract

 In this paper the design of an ATTITUDE CONTROL SYSTEM with REACTION JET is studied for a kind of vertical launch flying vehicle. The design process covers the components of the control system and the compensators. The ATTITUDE CONTROL SYSTEM controls the roll, pitch and yaw angles for a few seconds after the vertical launch. The system design is based on the desired time schedule and the maximum required pitch rate of the flying vehicle during the initial maneuver in the vertical plane. The compensators are designed based on the desired performance criteria as defined within the text. Finally the designed control system and controllers are evaluated using a variable mass 6DOF flight simulation utilizing the full nonlinear equations of motion and considering the saturation of control signals.

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    • Cite

    APA: Copy

    NOBAHARI, H., NOVIN ZADEH, A.B., & BANDIKENARI, H.. (2009). DESIGN OF A REACTION JET CONTROL SYSTEM FOR A VERTICAL LAUNCH FLYING VEHICLE. JOURNAL OF AEROSPACE SCIENCE AND RESEARCH, 2(2), 59-70. SID. https://sid.ir/paper/199476/en

    Vancouver: Copy

    NOBAHARI H., NOVIN ZADEH A.B., BANDIKENARI H.. DESIGN OF A REACTION JET CONTROL SYSTEM FOR A VERTICAL LAUNCH FLYING VEHICLE. JOURNAL OF AEROSPACE SCIENCE AND RESEARCH[Internet]. 2009;2(2):59-70. Available from: https://sid.ir/paper/199476/en

    IEEE: Copy

    H. NOBAHARI, A.B. NOVIN ZADEH, and H. BANDIKENARI, “DESIGN OF A REACTION JET CONTROL SYSTEM FOR A VERTICAL LAUNCH FLYING VEHICLE,” JOURNAL OF AEROSPACE SCIENCE AND RESEARCH, vol. 2, no. 2, pp. 59–70, 2009, [Online]. Available: https://sid.ir/paper/199476/en

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