18 research outputs found

    Suboptimal guidance with line-of-sight rate only measurements

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    Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76681/1/AIAA-1988-4066-823.pd

    Generalized guidance law for collision courses

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    Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76649/1/AIAA-21039-131.pd

    A Velocity and Distance Control System Synthesis Using Dynamic Inversion with PI Control

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    Modification of Augmented Proportional Navigation for a Missile with Varying Velocity

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    A Flight-Path Control of Aircraft Based on Required Acceleration Vector

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    A generalized guidance law for collision courses

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    Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76536/1/AIAA-1991-2782-100.pd

    Estimation of Missile Flight Distance and Guidance Law during Boost Phase

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    Advanced Pure Pursuit Guidance Via Sliding Mode Approach for Chase UAV

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    This paper introduces an advanced pure pursuit guidance method for chase UAV. The advanced pure pursuit guidance method employs a sliding mode approach using a proper Lyapunov function, which is based on a three-dimensional expression related to a line of sight (LOS) angle. In order to apply the sliding mode approach to the pure pursuit guidance, a simple surface vector and a derivation scheme from the sliding approach solution are also introduced. The guidance and control system employs the advanced pure pursuit guidance to determine the UAV\u27s commanded bank angle and angle of attack, and a two-time scaled dynamic inversion technique to control the attitude, which draws on the UAV\u27s high maneuverability and chasing capability. Copyright © 2009 by Takeshi Yamasaki and S.N. Balakrishnan

    Design of a Compensator for Proportional Navigation with .MU.-Synthesis

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