Implementation of optimal guidance laws using predicted missile velocity profiles

Journal of Guidance, Control, and Dynamics

Volumn 22, Issue 4, 1999, Pages 579-588

  Cho, Hangju ^a,c   Ryoo, Chang Kyung ^a   Tahk, Min Jea ^b,c  

^a Agency for Defence Development   (South Korea)

^b Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^c Department of Aerospace Engineering ^*  (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DRAG; EQUATIONS OF MOTION; MISSILES; OPTIMAL CONTROL SYSTEMS; VELOCITY;

DRAG MINIMIZATION PROBLEM; MISSILE VELOCITY PROFILE; WEIGHTED CONTROL EFFORT MINIMIZING GUIDANCE PROBLEM;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0032629006     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4420     Document Type: Article

References (5)

1. Baba, Y., Takehira, T., and Takano, H., "New Guidance Law for a Missile with Time Varying Velocity," Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Washington, DC, 1994, pp. 207-215.
2. Cho, H., Ryoo, C. K., and Tahk, M. J., "Closed-Form Optimal Guidance Law for Missiles of Time-Varying Velocity," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 5, 1996, pp. 1017-1022.
3. "Properties of a Standard Atmosphere," Item No. 77021, Engineering Science Data Unit, Royal Aeronautical Society, London, 1977.
4. Bryson, A. E., and Ho, Y. C., Applied Optimal Control, Wiley, New York, 1975, Chap. 5.
5. Ryoo, C. K., Cho, H., and Tahk, M. J., "Performance Characteristics of Linear Optimal Guidance Laws for Varying Velocity Missiles," Proceedings of 2nd Asian Control Conference (Seoul, Korea), Vol. 2, 1997, pp. 395-398.