Dynamic aircraft routing
A request for transport services that identifies a rider, an origin, and a destination is received from a client device. Eligibility of the request to be serviced by a vertical take-off and landing (VTOL) aircraft is determined based on the origin and the destination. A transportation system determines a first and a second hub for a leg of the transport request serviced by the VTOL aircraft and calculates a set of candidate routes from the first hub to the second hub. A provisioned route is selected from among the set of candidate routes based on network and environmental parameters and objectives including pre-determined acceptable noise levels, weather, and the presence and planned routes of other VTOL aircrafts along each of the candidate routes.
1 . A computer-implemented method for mitigating noise emissions from vertical take-off and landing (VTOL) aircraft, the method comprising:
computing a noise signature for a vertiport based on measured noise levels measured by a plurality of sensors of the vertiport; and
adjusting, based on the noise signature, a direction of a propeller of a VTOL aircraft at the vertiport as the VTOL aircraft transitions between a cruise state and a vertical take-off and landing state.
2 . The computer-implemented method of claim 1 , wherein the adjusting comprises:
outputting a command to a controller of the VTOL aircraft, the command operable to cause the VTOL aircraft to adjust the direction of transition.
3 . The computer-implemented method of claim 2 , wherein the VTOL aircraft transitions between the cruise state and the vertical take-off and landing state by controlling an angle of rotation of the propeller.
4 . The computer-implemented method of claim 1 , wherein the plurality of sensors comprise one or more microphones that are affixed at the vertiport.
5 . The computer-implemented method of claim 1 , wherein the plurality of sensors comprise one or more microphones that are fixed to, within the vicinity of the vertiport, at least one of: ground based infrastructure, a ground vehicle, an air vehicle, or a user device.
6 . The computer-implemented method of claim 1 , wherein the noise signature is computed based on a composite of distributed noise measurements from the plurality of sensors.
7 . A system for mitigating noise emissions from vertical take-off and landing (VTOL) aircraft, the system comprising:
a computing system having one or more processors and a memory operable to compute a noise signature for a vertiport based on measured noise levels measured by a plurality of sensors of the vertiport; and
a controller operable to adjust, based on the noise signature, a direction of a propeller of a VTOL aircraft at the vertiport as the VTOL aircraft transitions between a cruise state and a vertical take-off and landing state.
8 . The system of claim 7 , wherein the adjusting comprises:
outputting a command to a controller of the VTOL aircraft, the command operable to cause the VTOL aircraft to adjust the direction of transition.
9 . The system of claim 8 , wherein the VTOL aircraft transitions between the cruise state and the vertical take-off and landing state by controlling an angle of rotation of the propeller.
10 . The system of claim 7 , wherein the plurality of sensors comprise one or more microphones that are affixed at the vertiport.
11 . The system of claim 7 , wherein the plurality of sensors comprise one or more microphones that are fixed to, within the vicinity of the vertiport, at least one of: ground based infrastructure, a ground vehicle, an air vehicle, or a user device.
12 . The system of claim 7 , wherein the noise signature is computed based on a composite of distributed noise measurements from the plurality of sensors.
13 . A vertical take-off and landing (VTOL) aircraft comprising:
a propeller rotatable to transition between a cruise state and a vertical take-off and landing state; and
a controller operable to adjust, based on a noise signature for a vertiport based on measured noise levels measured by a plurality of sensors of the vertiport, a direction of the propeller as the VTOL aircraft transitions between the cruise state and the vertical take-off and landing state.
14 . The VTOL aircraft of claim 13 , wherein the controller is operable to receive a command to perform the adjusting and control, based on the command, the VTOL aircraft to control the direction of transition.
15 . The VTOL aircraft of claim 14 , wherein the VTOL aircraft receives the command from a computing system associated with the vertiport.
16 . The VTOL aircraft of claim 13 , comprising a computing system operable to output a command to a controller of the VTOL aircraft, the command operable to cause the VTOL aircraft to adjust the direction of transition.
17 . The VTOL aircraft of claim 13 , wherein the VTOL aircraft transitions between the cruise state and the vertical take-off and landing state by controlling an angle of rotation of the propeller.
18 . The VTOL aircraft of claim 17 , wherein a first angle of rotation of the propeller corresponds to a vertical thrust position and a second angle of rotation of the propeller corresponds to a forward thrust position.
19 . The VTOL aircraft of claim 13 , wherein the plurality of sensors comprise one or more microphones that are fixed to, within the vicinity of the vertiport, at least one of: ground based infrastructure, a ground vehicle, an air vehicle, or a user device.
20 . The VTOL aircraft of claim 13 , wherein the noise signature is computed based on a composite of distributed noise measurements from the plurality of sensors.