Roll-Pitch-Yaw Integrated H∞Controller Synthesis for High Angle-of-Attack Missiles
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چکیده
منابع مشابه
Roll-Pitch-Yaw Integrated Robust Autopilot Design for a High Angle-of-Attack Missile
This paper explores the feasibility of roll–pitch–yaw integrated autopilots for a high angle-of-attack missile. Investigation of the aerodynamic characteristics indicates strong cross-coupling effects between the motions in longitudinal and lateral directions. Robust control techniques based on H1 synthesis are employed to design roll– pitch–yaw integrated autopilots. The performance of the pro...
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Differential Game Based Guidance Law for High Angle of Attack Missiles By P. K. Menon and G.B. Chatterji Optimal Synthesis 450 San Antonio Road, Suite 53 Palo Alto, CA 94303 Abstract A nonlinear differential game theoretic intercept guidance law for short range missiles is derived. Differential geometric transformations are used to convert the nonlinear missile and the target models into a conv...
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Comparative misalignment disturbance functions (MDF) have been measured for rotations between display and control axes for pure pitch, roll, and yaw misalignments in a high fidelity virtual environment. Twenty participants manually moved a virtual cursor using position control to touch 3-dimensionally, randomly presented nearby targets having a constant Fitts Index of Difficulty. Results show a...
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ژورنال
عنوان ژورنال: International Journal of Aeronautical and Space Sciences
سال: 2008
ISSN: 2093-274X
DOI: 10.5139/ijass.2008.9.1.066