Mission monitor and controller for autonomous unmanned vehicles
First Claim
1. A flight control sending unit, comprising:
- at least one acoustic sensor attached to an aircraft, the acoustic sensor configured to sense an acoustic profile of the aircraft;
andat least one processor coupled by at least one system bus to the acoustic sensor and to a control system of the aircraft, the processor configured to;
(a) receive the sensed acoustic profile from the acoustic sensor;
(b) receive one or more of a position of the aircraft and an altitude of the aircraft via the system bus;
(c) determine a current flight segment of the aircraft based on the received position and the received altitude;
(d) determine an expected configuration of the aircraft corresponding to the current flight segment;
(e) determine a current configuration of the aircraft based on the sensed acoustic profile;
(f) determine at least one deviation of the current configuration from the expected configuration by comparing the expected configuration and the current configuration;
(g) detect at least one unusual condition associated with the current configuration by comparing the deviation to at least one threshold;
(h) if the at least one unusual condition is detected, generate one or more instructions corresponding to a configuration change, the one or more instructions associated with at least one of a configuration correction and an emergency configuration; and
(i) forward the one or more instructions to the control system.
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Accused Products
Abstract
A system and related method for monitoring the performance of one or more autonomous unmanned aircraft (UA) includes a flight assistant for periodically determining the viability of an aircraft flight command, flight, or mission by comparing expected flight segment configuration and performance against at least actual performance. The flight assistant may trend actual performance as a function of differences in expected position and actual position and determine whether a flight command, flight, or mission may be performed or continued according to a hierarchy of user selectable detected anomalies or safety concerns. The flight assistant may report to an operator, controller, pilot, or monitor a rate of deviation, size of deviation, or change in the rate of deviation in accordance with a hierarchy based at least in part on flight segment, altitude, proximity to people or things.
121 Citations
19 Claims
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1. A flight control sending unit, comprising:
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at least one acoustic sensor attached to an aircraft, the acoustic sensor configured to sense an acoustic profile of the aircraft; and at least one processor coupled by at least one system bus to the acoustic sensor and to a control system of the aircraft, the processor configured to; (a) receive the sensed acoustic profile from the acoustic sensor; (b) receive one or more of a position of the aircraft and an altitude of the aircraft via the system bus; (c) determine a current flight segment of the aircraft based on the received position and the received altitude; (d) determine an expected configuration of the aircraft corresponding to the current flight segment; (e) determine a current configuration of the aircraft based on the sensed acoustic profile; (f) determine at least one deviation of the current configuration from the expected configuration by comparing the expected configuration and the current configuration; (g) detect at least one unusual condition associated with the current configuration by comparing the deviation to at least one threshold; (h) if the at least one unusual condition is detected, generate one or more instructions corresponding to a configuration change, the one or more instructions associated with at least one of a configuration correction and an emergency configuration; and (i) forward the one or more instructions to the control system. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19)
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Specification