Dynamics and autopilot design for endoatmospheric interceptors with dual control systems

Author:

Zhou Di,Shao Chuntao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. W.R. Chadwick, Augmentation of high-altitude maneuver performance of a tailed-controlled missile using lateral thrust, AD-A328973

2. Y.S. Choi, H.C. Lee, J.W. Choi, Autopilot design for agile missile with aerodynamic fin and side thruster, in: Proceedings of the SICE Annual Conference in Fukui, Fukui, Japan, 2003, pp. 2188–2193

3. Three-axes missile autopilot design: from linear to nonlinear control strategies;Devaud;Journal of Guidance, Control, and Dynamics,2001

4. E. Devaud, H. Siguerdidjane, S. Font, Nonlinear dynamic autopilot design for the non-minimum phase missile, in: Proceedings of the 37th IEEE Conference on Decision & Control, Florida, USA, 1998, pp. 4691–4696

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