Aerospace Blockset Previous page   Next Page

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.


Previous page  Extending the Model NASA HL-20 Lifting Body Airframe Next page

Learn more about the latest releases of MathWorks products:

 © 1994-2009 The MathWorks, Inc.    -   Site Help   -   Patents   -   Trademarks   -   Privacy Policy   -   Preventing Piracy   -   RSS