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Integrated Roil-Pitch-Yaw Autopilot Design for Missiles
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 Title & Authors
Integrated Roil-Pitch-Yaw Autopilot Design for Missiles
Kim, Yoon-Hwan; Won, Dae-Yeon; Kim, Tae-Hun; Tahk, Min-Jea; Jun, Byung-Eul; Lee, Jin-Ik; An, Jo-Young;
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 Abstract
An roll-pitch-yaw integrated autopilot for missiles is designed for compensation of dynamics coupling. The proposed autopilot is based on the classical control technique. The gains of the proposed autopilot are optimized by using co-evolutionary augmented Lagrangian method(CEALM). Several cost functions are compared in order to find feasible control gains. For a case that a bank angle of missiles is unknown, multiple models are used in the autopilot optimization. In nonlinear simulations as well as linear simulations, the proposed autopilot provided good performances.
 Keywords
Autopilot design;Dynamics coupling; Missile;Parameter optimization;
 Language
English
 Cited by
1.
Three-Axis Autopilot Design for a High Angle-Of-Attack Missile Using Mixed H2/H Control,;;;

International Journal of Aeronautical and Space Sciences, 2010. vol.11. 2, pp.131-135 crossref(new window)
1.
Three-Axis Autopilot Design for a High Angle-Of-Attack Missile Using Mixed H2/H∞Control, International Journal of Aeronautical and Space Sciences, 2010, 11, 2, 131  crossref(new windwow)
 References
1.
W. R. Chadwick, 'Flight Dynamics of a bomb with cruciform Tail', Journal of Spacecraft, Vol.4, No. 6, pp. 768-773, June, 1967 crossref(new window)

2.
W. R. Chadwick, P. Zarchan, 'Interception of Spiraling Ballistic Missiles', Proceeding of the American Control Conference, Seattle, Washington, June, 1996

3.
B. L. Stevens and F. L. Lewis, Aircraft control and simulation, John Wiley & Sons, INC, 1992

4.
H. Ryu and M. J. Tahk, 'Automated Aircraft Flight Control Design Parameter Optimization Technique', KSAS Journal, pp. 111-119, 1998

5.
C. S. Park, J. Hur, and M. J. Tahk, 'Aircraft Control System Design Using Evolutionary Algorithm', KSAS Journal, pp. 104-114,1999

6.
Min-Jea Tahk and Byung-Chan Sun, 'Co-evolutionary augmented Lagrangian method for constrained optimization', IEEE Trans. on Evolutionary Computation, Vol. 4, No. 2, pp. 114-124, July, 2000 crossref(new window)