Adaptive sliding-mode guidance of a homing missile

Journal of Guidance, Control, and Dynamics

Volumn 22, Issue 4, 1999, Pages 589-594

  Zhou, Di ^a,b   Mu, Chundi ^a   Xu, Wenli ^a,c  

^a TSINGHUA UNIVERSITY   (China)

^b HARBIN INSTITUTE OF TECHNOLOGY   (China)

^c UNIVERSITY OF COLORADO   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; LINEAR CONTROL SYSTEMS; NONLINEAR CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); TIME VARYING CONTROL SYSTEMS;

ADAPTIVE SLIDING MODE GUIDANCE LAW; HOMING MISSILE; LINEAR TIME VARYING SYSTEM;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0032656126     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4421     Document Type: Article

References (4)

1. Gao, W. B., Fundamentals of Variable Structure Control Theory, 1st ed., Chinese Science and Technology Press, Beijing, 1990, pp. 24-37.
2. Brierley, S. D., and Longchamp, R., "Application of Sliding-Mode Control to Air-Air Interception Problem," IEEE Transactions on Aerospace and Electronic Systems, Vol. 26, No. 2, 1990, pp. 306-325.
3. Babu, K. R., Sarrna, I. G., and Swamy, K. N., "Switched Bias Proportional Navigation for Homing Guidance Against Highly Maneuvering Target," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 6, 1994, pp. 1357-1363.
4. Babu, K. R., Sarma, I. G., and Swamy, K. N., "Two Variable-Structure Homing Guidance Schemes With and Without Target Maneuver Estimation," AIAA Paper 94-3566, Aug. 1994.