Aircraft control method and apparatus and aircraft
First Claim
1. An aircraft, comprising:
- a light emitting apparatus; and
a processor configured to;
obtain ambient luminance data, wherein the ambient luminance data indicates ambient luminance of an environment;
determine whether the ambient luminance data satisfies a luminance value required for normal running of a vision system of the aircraft;
determine whether a flight height of the aircraft is less than a preset low-altitude height threshold; and
adjust a working status of the light emitting apparatus based on a determination that the ambient luminance data does not satisfy the luminance value required for normal running of the vision system and that the flight height is less than the preset low-altitude height threshold.
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Accused Products
Abstract
This invention discloses an aircraft control method, apparatus and an aircraft. The invention relates to the field of aircraft control technologies. The method includes: obtaining ambient luminance data by a luminance sensing apparatus of an aircraft; determining whether the ambient luminance data satisfies a luminance value required for normal running of a vision system of the aircraft; and adjusting, when the ambient luminance data does not satisfy the luminance value required for normal running of the vision system of the aircraft, a working status of a light emitting apparatus on the aircraft to change light emitting luminance of the light emitting apparatus. The foregoing aircraft control method, apparatus and the aircraft can accurately learn a flight environment in which the aircraft is located, thereby effectively implementing vision positioning on the aircraft and more conveniently controlling the aircraft.
16 Citations
30 Claims
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1. An aircraft, comprising:
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a light emitting apparatus; and a processor configured to; obtain ambient luminance data, wherein the ambient luminance data indicates ambient luminance of an environment; determine whether the ambient luminance data satisfies a luminance value required for normal running of a vision system of the aircraft; determine whether a flight height of the aircraft is less than a preset low-altitude height threshold; and adjust a working status of the light emitting apparatus based on a determination that the ambient luminance data does not satisfy the luminance value required for normal running of the vision system and that the flight height is less than the preset low-altitude height threshold. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16)
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17. An aircraft, comprising:
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a light emitting apparatus; and a processor configured to; determine whether a flight height of the aircraft is less than a preset low-altitude height threshold; determine whether the aircraft is in a low-light environment; adjust a working status of the light emitting apparatus based on a determination that the flight height is less than the preset low-altitude height threshold and that the aircraft is in the low-light environment. - View Dependent Claims (18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30)
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Specification