A new missile guidance algorithm against a maneuvering target

1998 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1998, Pages 145-153

  Imado, Fumiaki ^a   Kuroda, Takeshi ^b   Tahk, Min Jea ^c  

^a SHINSHU UNIVERSITY   (Japan)

^b MITSUBISHI ELECTRIC CORPORATION   (Japan)

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

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ELECTRONIC GUIDANCE SYSTEMS; GUIDED MISSILES; NAVIGATION;

AIRCRAFT MANEUVERS; AUGMENTED PROPORTIONAL NAVIGATION; GUIDANCE ALGORITHM; MANEUVERING TARGETS; PROPORTIONAL NAVIGATION; TARGET ACCELERATION ESTIMATION; TIME LAG;

AIR NAVIGATION;

EID: 84959145308     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4114     Document Type: Conference Paper

References (2)

1. Imado, F. and Miwa, S. "Missile Guidance Algorithm Against High-g Barrel Roll Maneuvers", Journal of Guidance, Control, and Dynamics, vol. 17, No. 1, pp. 123-128, 1994.
2. Imado, F., Kuroda, T. and Ichikawa, A. "A Trade-off Study Between Conventional And Augmented Proportional Navigation", AIAA paper 96-3882, AIAA Guidance Navigation and Control Conference, 1996.