Hyperstable range in homing missiles

Guidance, Navigation and Control Conference, 1990

Volumn , Issue , 1990, Pages 591-600

  Tanaka, Toshiyuki ^a   Eguchi, Hirofumi ^a  

^a JAPAN DEFENSE AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

DIGITAL COMPUTERS;

DESIGN VARIABLES; HOMING MISSILE; HYPERSTABILITY; INITIAL SITUATION; MISS DISTANCE; NYQUIST;

MISSILES;

EID: 84999048275     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1990-3381     Document Type: Conference Paper

References (12)

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2. Gamell, P., “Guided Weapon Control Systems”, Brassey’s Defence Publishers, 1980, PP. 185-241
3. Tanaka, T. and Eguchi, H., “Essential Instability in Homing Missiles”, JSASS 27th Aircraft Symposium, 1989, pp. 296-299.
4. Bonenn, Z. and Shneydor, N., “Divergence Range in a Proportional-Navigation Honing System”, Israel Journal of Technology, vol, 5, 1967, pp. 129-139.
5. Nesline, F. W., “Missile Guidance for Law-Altitude Air Defense”, Journal of Guidance and Control, vol, 2, 1979, pp. 283-289.
6. Nesline, F. W. and Zarchan, P,“Missile Guidance Design Tradeoffs for High-Altitude Air Defense”, Journal of Guidance and Control, vol. 6, 1983
7. Eguchi, H. and Watanafce, K, “Properties of Internally Stabilized Tracking Seeker Mounted on a Guided Missile”, TRDI TR-5472, 1989.
8. Tanaka, T. and Eguchi, H., “A Design of Robust Regulator Eased on Matrix Norms”, TRDI TR-5464, 1989.
9. Popov, V. H., “The Solution to a New Stability Problem for Controlled Systems”, Automation and Remote Control, vol, 24, 1963, pp. 1-23.
10. Popov, V. H., “Hyperstability of Control Systems”, Springer-Verlag, 1973, pp. 118-239.
11. Desor, C. A, and Vidyasagar, M., “Feedback Systems: Input-Cutput Properties”, Academic press, 1975
12. Tanaka, T and Eguchi, K., “Hyperstable Minimum Range of Homing Missiles”, TRDI TR-5628, 1989.