ANALYTICAL METHOD FOR CALCULATING START TIME OF TERMINAL GUIDANCE IN ORDER TO ACHIEVING PROPER IMPACT ANGLE IN A TACTICAL MISSILE

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TAGHIPOUR KAMANI A.; AARAVAN M.R.; MOHAMMADI A.

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Journal: Journal of Control Year:2009 | Volume:3 | Issue:3 Page(s): 1-8

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Title

ANALYTICAL METHOD FOR CALCULATING START TIME OF TERMINAL GUIDANCE IN ORDER TO ACHIEVING PROPER IMPACT ANGLE IN A TACTICAL MISSILE

Author(s)

TAGHIPOUR KAMANI A. | AARAVAN M.R. | MOHAMMADI A. | Issue Writer Certificate

Keywords

BIASED TRUE PROPORTIONAL NAVIGATION (BTPN)Q3

TERMINAL PHASEQ3

IMPACT ANGLE TO TARGETQ3

Abstract

The TERMINAL PHASE is an intercept phase. Missile performance is dependent on: guidance law, seeker accuracy, impact angle. Impact angle should be control for most performance of warhead in target destruction. A great impact angle is not achievable because of some limitations. Start time of TERMINAL PHASE is significant parameter for control of impact angle in case of surface target such as tanks and ships. This time determines IMPACT ANGLE TO TARGET and missile impact to ground avoidance before impact to target. This paper presents an algorithm to determination start time of TERMINAL PHASE by using of biased true proportional navigation guidance and approximation of impact angle so that controls final impact angle. Maximum value of impact angle analyzes and conditions of solution existence for purposed algorithm to achieve desired impact angle is determined with a theorem declaration and proof.

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APA: Copy

TAGHIPOUR KAMANI, A., AARAVAN, M.R., & MOHAMMADI, A.. (2009). ANALYTICAL METHOD FOR CALCULATING START TIME OF TERMINAL GUIDANCE IN ORDER TO ACHIEVING PROPER IMPACT ANGLE IN A TACTICAL MISSILE. JOURNAL OF CONTROL, 3(3), 1-8. SID. https://sid.ir/paper/120820/en

Vancouver: Copy

TAGHIPOUR KAMANI A., AARAVAN M.R., MOHAMMADI A.. ANALYTICAL METHOD FOR CALCULATING START TIME OF TERMINAL GUIDANCE IN ORDER TO ACHIEVING PROPER IMPACT ANGLE IN A TACTICAL MISSILE. JOURNAL OF CONTROL[Internet]. 2009;3(3):1-8. Available from: https://sid.ir/paper/120820/en

IEEE: Copy

A. TAGHIPOUR KAMANI, M.R. AARAVAN, and A. MOHAMMADI, “ANALYTICAL METHOD FOR CALCULATING START TIME OF TERMINAL GUIDANCE IN ORDER TO ACHIEVING PROPER IMPACT ANGLE IN A TACTICAL MISSILE,” JOURNAL OF CONTROL, vol. 3, no. 3, pp. 1–8, 2009, [Online]. Available: https://sid.ir/paper/120820/en

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