2007Modern Defence TechnologyRequires access

Trajectory Design Research of Anti-warship Missile with Combination of Maneuver and Guidance

Sun Mingwei

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Abstract

Conventional maneuver and guidance of anti-warship missile are designed seperately,thus the penetration effect is limited.To achieve dual goals of increasing penetration probability and maintaining high-precision guidance,the anti-warship missile's terminal combination of maneuver and guidance should be adopted.In view of geometry relation of missile and target,reference command of adaptive snaking maneuver was obtained based on real-time missile-target connection line.The whole design may be regarded as a composition of proportional navigation with snaking maneuvering.The available data are real-time azimuth angle,missile-target distance and specified time series signal.

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What this paper is about

Conventional maneuver and guidance of anti-warship missile are designed seperately,thus the penetration effect is limited.To achieve dual goals of increasing penetration probability and maintaining high-precision guidance,the anti-warship missile's terminal combination of maneuver and guidance should be adopted.In view of geometry relation of missile and target,reference command of adaptive snaking maneuver was obtained based on real-time missile-target connection line.The whole design may be regarded as a composition of proportional navigation with snaking maneuvering.The available data are real-time azimuth angle,missile-target distance and specified time series signal.

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Available abstract

Conventional maneuver and guidance of anti-warship missile are designed seperately,thus the penetration effect is limited.To achieve dual goals of increasing penetration probability and maintaining high-precision guidance,the anti-warship missile's terminal combination of maneuver and guidance should be adopted.In view of geometry relation of missile and target,reference command of adaptive snaking maneuver was obtained based on real-time missile-target connection line.The whole design may be regarded as a composition of proportional navigation with snaking maneuvering.The available data are real-time azimuth angle,missile-target distance and specified time series signal.

Key concepts: Missile, Terminal guidance, Missile guidance, Trajectory, Engineering, Azimuth, Guidance system, Proportional navigation

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