Agile Missile Autopilot Design using Nonlinear Backstepping Control with Time-Delay Adaptation

Author:

LEE Chang-Hun,KIM Tae-Hun,TAHK Min-Jea

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference29 articles.

1. 1) Wise, K. A. and Broy, D. J.: Agile Missile Dynamics and Control, J. Guid. Control Dynam., 21, 3 (1998), pp. 441–449.

2. 2) Thukral, A. and Innocenti, M.: A Sliding Mode Missile Pitch Autopilot Synthesis for High Angle of Attack Maneuvering, IEEE Trans. Control Syst. Technol., 6, 3 (1998), pp. 359–371.

3. 3) Leith, D. J., Tsourdos, A., White, B. A. and Leithead, W. E.: Application of Velocity-Based Gain-Scheduling to Lateral Auto-Pilot Design for an Agile Missile, Control Eng. Practice, 9 (2001), pp. 1079–1093.

4. 4) Kang, S. H., Kim, H. J., Lee, J. I., Jun, B. E. and Tank, M. J.: Roll-Pitch-Yaw Integrated Robust Autopilot Design for a High Angle-of-Attack Missile, J. Guid. Control Dynam., 32, 5 (2009), pp. 1622–1628.

5. 5) Buschek, H.: Full Envelope Missile Autopilot Design Using Gain Scheduled Robust Control, J. Guid. Control Dynam., 22, 1 (1999), pp. 115–122.

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