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Journal of Guidance Control and Dynamics

Volumn 24, Issue 3, 2001, Pages 452-459

Neoclassical guidance for homing missiles

(3) Gurfil, Pini a Jodorkovsky, Mario b Guelman, Moshe c

a Princeton University (United States)

b RAFAEL (Israel)

c TECHNION ISRAEL INSTITUTE OF TECHNOLOGY (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; DISTANCE MEASUREMENT; KINEMATICS; LINEARIZATION; MANEUVERABILITY; RANDOM PROCESSES; TRANSFER FUNCTIONS;

HOMING MISSILES; LINE OF SIGHT RATE MEASUREMENT; NEOCLASSICAL GUIDANCE; PROPORTIONAL NAVIGATION; ZERO MISS DISTANCE;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0035335177 PISSN: 07315090 EISSN: None Source Type: Journal
DOI: 10.2514/2.4765 Document Type: Article

Times cited : (45)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.