Methods and apparatus of notification of a flight asymmetry influencing an aircraft
First Claim
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1. A method for alerting a pilot of an aircraft of a flight asymmetry influencing the aircraft, the method comprising:
- monitoring a roll characteristic of the aircraft;
determining an output of an autopilot system of the aircraft to control the roll characteristic;
determining an amount of authority utilized by the autopilot system to control the roll characteristic;
determining whether the aircraft is influenced by a first condition based on the output and the amount of authority, the first condition indicative of the flight asymmetry;
detecting a second condition of at least one of the autopilot system or the aircraft, the second condition different from the first condition;
determining whether the second condition indicates a presence or an absence of a predetermined condition for the at least one of the autopilot system or the aircraft;
when the second condition indicates the presence or the absence of the predetermined condition, enabling communication of an instruction to generate an alert;
communicating the instruction to generate the alert when (1) the aircraft is influenced by the first condition and (2) communication of the instruction to generate the alert is enabled based on the second condition; and
generating the alert based on the instruction, the alert including a graphic to be displayed via a cockpit display, the graphic indicating one or more of a correction the pilot of the aircraft is to take or a direction in which the pilot is to rotate a yoke of the aircraft.
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Abstract
Methods and apparatus of notification of a flight asymmetry influencing an aircraft are disclosed herein. An example method includes monitoring a roll characteristic of an aircraft and determining an output of an autopilot system of the aircraft to control the roll characteristic. The example method further includes generating an alert based on the output and an authority of the autopilot system to control the roll characteristic.
19 Citations
23 Claims
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1. A method for alerting a pilot of an aircraft of a flight asymmetry influencing the aircraft, the method comprising:
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monitoring a roll characteristic of the aircraft; determining an output of an autopilot system of the aircraft to control the roll characteristic; determining an amount of authority utilized by the autopilot system to control the roll characteristic; determining whether the aircraft is influenced by a first condition based on the output and the amount of authority, the first condition indicative of the flight asymmetry; detecting a second condition of at least one of the autopilot system or the aircraft, the second condition different from the first condition; determining whether the second condition indicates a presence or an absence of a predetermined condition for the at least one of the autopilot system or the aircraft; when the second condition indicates the presence or the absence of the predetermined condition, enabling communication of an instruction to generate an alert; communicating the instruction to generate the alert when (1) the aircraft is influenced by the first condition and (2) communication of the instruction to generate the alert is enabled based on the second condition; and generating the alert based on the instruction, the alert including a graphic to be displayed via a cockpit display, the graphic indicating one or more of a correction the pilot of the aircraft is to take or a direction in which the pilot is to rotate a yoke of the aircraft. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 20, 21)
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9. A method for alerting a pilot of an aircraft of a flight asymmetry influencing the aircraft, the method comprising:
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determining a flight characteristic of the aircraft; determining output of an autopilot system of the aircraft to control the flight characteristic; determining an amount of roll authority utilized by the autopilot system of the aircraft; determining whether the aircraft is influenced by a first condition based on the output and the amount of authority, the first condition indicative of the flight asymmetry; detecting a second condition of at least one of the autopilot system or the aircraft, the second condition different from the first condition; determining whether the second condition indicates a presence or an absence of a predetermined condition for the at least one of the autopilot system or the aircraft; when the second condition indicates the presence or the absence of the predetermined condition, enabling communication of an instruction to generate an alert; communicating the instruction to generate the alert when (1) the aircraft is influenced by the first condition and (2) communication of the instruction to generate the alert is enabled based on the second condition; and generating the alert based on the instruction, the alert including a graphic to be displayed via a cockpit display, the graphic indicating one or more of a correction the pilot of the aircraft is to take or a direction in which the pilot is to rotate a yoke of the aircraft. - View Dependent Claims (10, 11, 12, 13, 14, 22)
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15. A method for alerting a pilot of an aircraft of a flight asymmetry influencing the aircraft, the method comprising:
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determining an amount of roll authority utilized by an autopilot system of the aircraft to provide an output; monitoring a flight characteristic of the aircraft; monitoring the output to control the flight characteristic; determining whether the aircraft is influenced by a first condition based on the output and the amount of roll authority, the first condition indicative of the flight asymmetry; detecting a second condition of at least one of the autopilot system or the aircraft, the second condition different from the first condition; determining whether the second condition indicates a presence or an absence of a predetermined condition for the at least one of the autopilot system or the aircraft; when the second condition indicates the presence or the absence of the predetermined condition, enabling communication of an instruction to generate an alert; communicating the instruction to generate the alert when (1) the aircraft is influenced by the first condition and (2) communication of the instruction to generate the alert is enabled based on the second condition; and generating the alert based on the instruction, the alert including a graphic to be displayed via a cockpit display, the graphic indicating one or more of a correction the pilot of the aircraft is to take or a direction in which the pilot is to rotate a yoke of the aircraft. - View Dependent Claims (16, 17, 18, 19, 23)
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Specification