Assisted takeoff
DCFirst Claim
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1. A method of assisted takeoff of an aerial vehicle, said method comprising:
- increasing output to an actuator of the aerial vehicle under a first control scheme, wherein the output to the actuator results in the increase of an altitude of the aerial vehicle;
determining, with aid of a processor, whether the aerial vehicle has met a takeoff threshold based on the output to the actuator, the output measured from the actuator, or velocity or acceleration of the aerial vehicle, wherein determining whether the aerial vehicle has met the takeoff threshold is performed without (1) using signals from a source external to the aerial vehicle, or (2) using signals reflected to the aerial vehicle; and
controlling the output to the actuator using a second control scheme when the aerial vehicle has met the takeoff threshold.
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Abstract
Systems, methods, and devices are provided for assisted takeoff of an aerial vehicle. The aerial vehicle may takeoff using a first control scheme and switch to a second control scheme for normal flight when a takeoff threshold is met. The first control scheme optionally does not use integral control while the second control scheme may use integral control. The aerial vehicle may determine that a takeoff threshold is met, based on an output to a motor of the aerial vehicle and/or an acceleration of the aerial vehicle.
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30 Claims
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1. A method of assisted takeoff of an aerial vehicle, said method comprising:
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increasing output to an actuator of the aerial vehicle under a first control scheme, wherein the output to the actuator results in the increase of an altitude of the aerial vehicle; determining, with aid of a processor, whether the aerial vehicle has met a takeoff threshold based on the output to the actuator, the output measured from the actuator, or velocity or acceleration of the aerial vehicle, wherein determining whether the aerial vehicle has met the takeoff threshold is performed without (1) using signals from a source external to the aerial vehicle, or (2) using signals reflected to the aerial vehicle; and controlling the output to the actuator using a second control scheme when the aerial vehicle has met the takeoff threshold. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17)
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18. A system for assisted takeoff of an aerial vehicle, said system comprising:
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an actuator of the aerial vehicle, wherein an output to the actuator results in the increase of an altitude of the aerial vehicle; and one or more processors, individually or collectively configured to; (a) determine whether the aerial vehicle has met a takeoff threshold based on the output to the actuator, the output measured from the actuator, or velocity or acceleration of the aerial vehicle, wherein said determination whether the aerial vehicle has met the takeoff threshold is performed without (1) using signals from a source external to the aerial vehicle, or (2) using signals reflected to the aerial vehicle, and (b) generate a signal used to control the output to the actuator (1) using a first control scheme when the aerial vehicle has not met the takeoff threshold, and (2) using a second control scheme when the aerial vehicle has met the takeoff threshold. - View Dependent Claims (19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30)
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Specification