Carlee A. Bishop
Abstract
An integral guidance technique is proposed which uses the line-of-sight angle, as well as line-of-sight rate to determine the guidance command. Integral guidance is compared with proportional navigation guidance in a ballistic missile application and is found to reduce trajectory dispersions caused by disturbances.
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An integral guidance technique is proposed which uses the line-of-sight angle, as well as line-of-sight rate to determine the guidance command. Integral guidance is compared with proportional navigation guidance in a ballistic missile application and is found to reduce trajectory dispersions caused by disturbances.
Key concepts: Ballistic missile, Line-of-sight, Missile guidance, Guidance system, Trajectory, Proportional navigation, Missile, Trajectory of a projectile