Patent
Fourth order predictive, augmented proportional navigation system terminal guidance design with missile/target decoupling
TLDR
In this article, the authors proposed a method for augmenting a noise-adaptive predictive proportional navigation terminal guidance scheme with target and missile information terms and a navigation ratio which is a function of time-to-go.Citations
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Patent
Self-adaptive IRU correction loop design interfacing with the target state estimator for multi-mode terminal handoff
TL;DR: In this paper, a method and apparatus for identifying inertial reference unit (IRU) errors in a guided missile employing a multi-mode guidance system and constructing correction terms to recover the missile true position is presented.
Patent
Advanced homing guidance system and method
TL;DR: In this article, a line-of-sight rod is treated as a collapsible rod which is connected at one end through a mechanical gimbal set, and connected at the other end by a universal joint with four degrees of freedom.
Patent
Method for station keeping control of flexible spacecraft using onboard gain scheduling scheme
John F. Yocum,Dan Y Liu +1 more
TL;DR: In this article, a method of attitude control for spacecraft with flexible structures utilizes an estimator/state controller pair with on-board time-varying gain scheduling, where the estimator employs a predictor-corrector structure which computes initial rate and position estimates for each sample interval and corrects these values by weighing them with iteratively-calculated time varying gains according to equations 35 and 36.
Patent
System and method for periodically adaptive guidance and control
TL;DR: In this paper, a system and method that guides a device to an object using periodically adaptive guidance is presented, where a set of harmonically balanced Kalman filter banks are used to estimate the periodic maneuver of evasive objects.
Patent
Radar tracking system
TL;DR: In this article, a radar tracking system for an anti-aircraft, missile, including angle tracking, doppler tracking and range tracking feedback loops operating on sum and difference channels is presented.
References
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Patent
Kalman estimator tracking system
TL;DR: In this article, a radar tracking system with a Kalman estimator is described, which is provided with angle and range track error measurements in a coordinate system that is aligned with and normal to the antenna line of sight, commonly referred to as the LOS coordinate system.
Patent
Prediction computation for weapon control
TL;DR: In this paper, a target tracking sensor mechanization is provided which generates target position, velocity, and acceleration data components in an inertially-stabilized Cartesian coordinate system, whereby improved closed-loop pilot-aircraft weapon control system dynamic stability and accuracy result are also obtained by virtue of such inertially stabilized tracking mechanization.
Patent
System for estimating acceleration of maneuvering targets
TL;DR: In this paper, the attenuation inherent in the practical estimation of target acceleration is effectively removed for severely maneuvering targets by a compensating system that provides an attenuation factor, and multiplies the estimated acceleration output signal by the reciprocal of such factor.
Patent
System for tracking a moving target with respect to a frame of reference of unvarying orientation and fixed origin relative to earth
TL;DR: In this paper, the tracking system is provided with a device for measuring the position of the target in relation to the carrier and with a servocontrol unit for servo controlling the aiming of the device.
Patent
Body referenced gimballed sensor system
Donald E. Cole,John M. Speicher +1 more
TL;DR: In this article, a system for proportionally navigating an airframe to a target wherein the airframe is maneuvered by an onboard flight control system including body rate gyros is presented.