Optimal Orientation Controller Design for F-16/MATV Using Robust and Discrete Linear–Quadrature–Gaussian (LQG) Controller

Author:

Kassahun Berisha G.,Kumar Parvendra

Publisher

Springer Singapore

Reference23 articles.

1. Yang S (1996) Analysis of optimal midcourse guidance law. IEE Trans Aerosp Electron Syst 32(1):419–425

2. Dozwerneman W, Eller BG (1994) VISTA/F-16 multi axis thrust vectoring (MATV) control law design and evaluation. Lockheed Fort Worth Company, 13 July 1994

3. Wikipeda, Linear-quadratic-gaussian-control (online). Available http://en.wikipedia.org/wiki/Linearquadratic-Gaussian_control. Accessed 3 1 2018

4. Labane C, Zemalache MK (2014) Aircraft control system using LQG and LQR controller with optimal estimation-Kalman filter design. In: 3rd international symposium on aircraft airworthiness, ISAA 2013, no 80, pp 245–257

5. Sonneveldt L, Chu QP, Mulder JA (2007) Nonlinear flight control design using constrained adaptive backstepping. J Guid Control Dyn 324–325

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