Recursive time-to-go estimation for homing guidance missiles

IEEE Transactions on Aerospace and Electronic Systems

Volumn 38, Issue 1, 2002, Pages 13-24

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

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

^b Agency for Defence Development   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

HOMING GUIDANCE MISSILES; RECURSIVE METHOD; RECURSIVE TIME TO GO ESTIMATION; TIME TO GO ERROR;

COMPUTATIONAL METHODS; ELECTRONIC GUIDANCE SYSTEMS; ERROR COMPENSATION; ESTIMATION; NAVIGATION; RECURSIVE FUNCTIONS; VELOCITY;

MISSILES;

EID: 0036250583     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.993225     Document Type: Article

References (11)

1. Linear optimal guidance for short range air-to-air missiles
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5. New guidance law for a missile with time varying velocity
6. Closed-form optimal guidance law for missiles of time-varying velocity
7. Optimal planar interception with fixed end conditions: Closed-form solution
8. Optimal guidance with reduced sensitivity to time-to-go estimation errors
9. Optimal pure proportional navigation for maneuvering targets
10. Biased PNG law for impact with angular constraint
11. Implementation of optimal guidance laws using predicted missile velocity profiles