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Application of improved L2-gain synthesis on LPV missile autopilot design

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2 Author(s)
Sungyung Lim ; Dept. of Aeronaut. & Astronaut., Stanford Univ., CA, USA ; How, J.P.

Presents an improved finite-dimensional linear matrix inequality (LMI) formulation for the L2-gain synthesis of a piecewise-affine linear parameter-varying (PALPV) system. The new formulation is then used to design a missile autopilot to investigate issues such as the effectiveness, reliability, and conservatism. Our approach is based on a nonsmooth dissipative systems framework using a continuous, quasi-piecewise-affine parameter-dependent Lyapunov function (QPAL) which has been shown to yield a less conservative, guaranteed result than previously published techniques based on quasi-affine parameter-dependent Lyapunov functions (QALs) or Lure-Postnikov Lyapunov functions. The results in the paper improve the computational efficiency by using a different “convexifying” technique. We also generalize our previous results by eliminating the restriction on the number of parameters

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American Control Conference, 1999. Proceedings of the 1999  (Volume:6 )

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