Augmented proportional navigation in second order predictive sch

Electricity: motive power systems – Positional servo systems – Adaptive or optimizing systems including 'bang-bang' servos

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244 314, 244 316, 244 317, 244 319, 364453, 364456, 364462, 318580, 318584, G05B 1300

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active

044568622

ABSTRACT:
A method for augmenting a noise-adaptive predictive proportional navigation terminal guidance scheme. In a second order configuration with noise adaptive varying gain parameters calculated as a function of time-to-go, this system implements an optimal control law to augment proportional navigation with a missile acceleration feedback term and a navigation ratio to account for first order autopilot time lag. This configuration results in nearly optimal miss distance behavior, with sensitivity to unmodeled errors being substantially less than that in modern guidance systems. The system is particularly useful for high altitude, minimally maneuvering targets.

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Price et al., "Direct Statistical Evaluation of Nonlinear Guidance Systems", AIAA Guidance and Control Conference, 8/22/73.

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