Autopilot Design Using Hybrid PSO-SQP Algorithm
Author:
Publisher
Springer Berlin Heidelberg
Link
http://link.springer.com/content/pdf/10.1007/978-3-540-74282-1_67.pdf
Reference16 articles.
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3. Thukral, A., Innocenti, M.: A Sliding Mode Missile Pitch Autopilot Synthesis for High Angle of Attack Maneuvering. IEEE Transaction on Control Systems Technique 6(3) (1998)
4. Kim, S., Kim, Y., Song, C.: A Robust Adaptive Nonlinear Control Approach to Missile Autopilot Design. Control Engineering Practice 12(2) (2004)
5. Farrell, J., Sharma, M., Polycarpou, M.: Backstepping-Based Flight Control with Adaptive Function Approximation. Journal of Guidance, Control, and Dynamics 24(3) (2005)
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