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Accurate Automation Corporation

Chadwick James Cox

Carl Edwin Lewis, Iii

An invention was developed to improve the performance and survivability of units in a competitive environment. Cryptic Command, Control, and Planning, and Management increases to apparent randomness of a plan from an opponent's perspective without increasing the randomness that is apparent to friendly parties. Friendly systems each carry a keyed pseudo-random or chaotic number generating process and a known method for mapping the numbers to behavioral modifications. Since the opponent does not know the key, the sequence, or the mapping, the result from his point of view is increased randomness and degraded predictive capability. Since friendly systems know each other's key, sequence, and mapping, they can predict each other's behavior or generate compatible controls or plans. This improves coordination of friendly units while forcing the opponent to revert to reactive responses rather than maintaining predictive responses. The process is less sensitive to communications degradation than are standard methods of maintaining coordination. This is because communications are only required when elements of the situation change and when these changes are not sensed by all the parties being coordinated.

Cryptic information and behavior generation for competitive environments

The apparatus of this invention includes a pilot-induced oscillation (PIO) detector, a PIO compensator and a pilot input modifier. The PIO detector is coupled to receive aircraft state signal including the aircraft's pitch, roll and yaw attitudes. The PIO detector is also coupled to receive pilot control signal generated by the aircraft's pilot by manipulation of flight control instruments. Preferably, the PIO detector includes a feature calculator and a discriminator. Based on the aircraft state signal and the pilot control signal, the feature calculator generates at least one feature signal indicative of whether a PIO or non-PIO condition exists in the aircraft. The feature calculator supplies the feature signal to the discriminator, that uses the feature signal to determine whether or not a PIO condition exists. The discriminator preferably uses a discrimination function determined by a neural network trained to discriminate PIO and non-PIO conditions, to generate the PIO indicator signal based on the feature signal(s). The discriminator generates the PIO indicator signal that indicates the likelihood of the existence of a PIO condition in the aircraft. The PIO indicator signal can be coupled to an audio and/or visual alarm to warn the pilot that the pilot's control actions are driving the PIO condition. The PIO compensator is coupled to receive the PIO indicator signal, and generates the compensation signal using the PIO indicator signal. The PIO compensator is coupled to output the PIO compensation signal to a pilot input modifier. In addition to the compensation signal, the pilot input modifier receives and modifies the pilot control signal, based on the compensation signal. The pilot input modifier can accomplish appropriate modification through gain attenuation or phase shift of the pilot control signal. The modified pilot control signal is used to control the aircraft's flight control actuators to eliminate the PIO condition. Accordingly, the invented apparatus prevents aircraft damage or pilot injury or death, that could otherwise result from a PIO condition. The invention also includes a related method.

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Chattanooga, TN, United States of America

Chadwick James Cox