Vehicle-based automatic traffic conflict and collision avoidance
First Claim
1. A method for aircraft guidance, comprising:
- determining a first flight trajectory for a first aircraft;
determining a second flight trajectory for a second aircraft;
predicting a distance between the first aircraft and the second aircraft at a closest point of approach (CPA) based on the first and second flight trajectories;
establishing a three-dimensional separation perimeter layer that provides at least one minimum separation distance from the first aircraft to the second aircraft, each dimension in the three-dimensional separation perimeter layer corresponding to a respective control direction having an avoidance gain;
comparing the distance to the three-dimensional separation perimeter layer; and
altering the first flight trajectory based at least on an avoidance control command having a magnitude that includes gain contribution from the avoidance gain of each dimension when the predicted distance breaches the three-dimensional separation perimeter layer.
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Accused Products
Abstract
Systems and methods for providing vehicle-centric collision avoidance are disclosed. In one embodiment, a method includes determining a first flight trajectory for a first aircraft. The method also includes determining a second flight trajectory for a second aircraft. A distance between the first aircraft and the second aircraft at a first closest point of approach (CPA) is predicted. The predicted closest point of approach is then compared to a separation perimeter layer. The separation perimeter layer is configured to provide a minimum separation distance from the first aircraft to the second aircraft. When the predicted closest point of approach breaches the separation perimeter, the first flight trajectory is altered to provide collision avoidance.
57 Citations
15 Claims
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1. A method for aircraft guidance, comprising:
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determining a first flight trajectory for a first aircraft; determining a second flight trajectory for a second aircraft; predicting a distance between the first aircraft and the second aircraft at a closest point of approach (CPA) based on the first and second flight trajectories; establishing a three-dimensional separation perimeter layer that provides at least one minimum separation distance from the first aircraft to the second aircraft, each dimension in the three-dimensional separation perimeter layer corresponding to a respective control direction having an avoidance gain; comparing the distance to the three-dimensional separation perimeter layer; and altering the first flight trajectory based at least on an avoidance control command having a magnitude that includes gain contribution from the avoidance gain of each dimension when the predicted distance breaches the three-dimensional separation perimeter layer. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14)
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15. A method comprising:
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determining a first flight trajectory for a first aircraft; determining a second flight trajectory for a second aircraft; predicting a distance between the first aircraft and the second aircraft at a closest point of approach (CPA) based on the first and second flight trajectories; providing at least one avoidance control command to a flight control of the first aircraft to alter the first flight trajectory when a time duration to arrive at the CPA for the first aircraft reaches a predetermined time threshold, the avoidance control command having a magnitude that includes a gain contribution from an avoidance gain of each dimension; and delaying the at least one avoidance control command to a flight control of the first aircraft to alter the first flight trajectory when the time duration to arrive at the CPA is longer than the predetermined time threshold.
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Specification