| Aerospace Blockset | ![]() |
References
[1] Bennani, S., D. M. C. Willemsen, and C. W. Scherer, "Robust LPV control with bounded parameter rates," AIAA-97-3641, August 1997.
[2] Mracek, C. P. and J. R. Cloutier, "Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method," AIAA-97-3767, August 1997.
[3] Shamma, J. S. and J. R. Cloutier, "Gain-Scheduled Missile Autopilot Design Using Linear Parameter Varying Transformations," Journal of Guidance, Control and Dynamics, Vol. 16, No. 2, March-April 1993.
[4] Lin, Ching-Fang, Modern Navigation, Guidance, and Control Processing, Volume 2, ISBN 0-13-596230-7, Prentice Hall, 1991.
| Extending the Model | NASA HL-20 Lifting Body Airframe | ![]() |
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