Helicopter ground movement system and method
Disclosed is a ground movement system for a helicopter having a fuselage and rotor blades fixed to the top of the fuselage, the ground movement system comprising at least three wheels secured below the fuselage of the helicopter, the wheels being retractable during flight; a motor positioned in the hub or on the undercarriage leg of each of at least two of the wheels, wherein each motor is operable to rotate the wheel in forward and backward directions; wherein each motor allows the wheel to rotate freely when unpowered; at least one user interface operable to receive user input commands to control the speed and direction of travel of the helicopter using the ground movement system; and a control arrangement to provide control signals to each of the motors based on the user input commands.
1. A ground movement system for a helicopter having a fuselage and rotor blades fixed to the top of the fuselage, the ground movement system comprising:
at least three wheels secured below the fuselage of the helicopter, the wheels being retractable during flight;
a motor positioned in the hub or on the undercarriage leg of each of at least two of the wheels;
wherein each motor is operable to rotate the wheel in forward and backward directions;
wherein each motor allows the wheel to rotate freely when unpowered;
at least one user interface operable to receive user input commands to control the speed and direction of travel of the helicopter using the ground movement system; and
a control arrangement to provide control signals to each of the motors based on the user input commands,
wherein the control arrangement is operable to determine differential control signals for each motor based on user input commands to control the direction of travel according to the user input commands,
wherein the at least one user interface comprises a helicopter user interface fixed within the helicopter cockpit and comprising a projecting user interface element movable between an up position and a down position,
wherein in the up position the projecting user interface element protrudes from a surface of the helicopter user interface and is operable as at least one of a speed and steering controller for the ground movement system of the helicopter,
wherein the projecting user interface element is tiltable to receive user input when in the up position but not when in the down position.
2. A helicopter ground movement system according to claim 1 , further comprising a motor power source for the motors separate from the power source for the rotor blades of the helicopter.
3. A helicopter ground movement system according to claim 2 , wherein the motor power source is an electrical battery power source, optionally detachable from the helicopter.
4. A helicopter ground movement system according to claim 3 , wherein the electrical battery power source is chargeable using energy generated by an engine of the helicopter.
5. A helicopter ground movement system according to claim 3 , further comprising a switching arrangement for selectively connecting the motor power source to a charging circuit to be charged by energy generated by an engine of the helicopter; and for disconnecting the electrical battery power source(s) from the charging circuit when the engine is not providing electrical power.
6. A helicopter ground movement system according to claim 1 , wherein each motor is not more than 20 cm thick, and not more than 20 cm in diameter, preferably not more than 15 cm thick.
7. A helicopter ground movement system according to claim 1 , further comprising:
a brake for each of the wheels, preferably located within the wheel hubs; and
wherein the control arrangement is operable to provide control signals to the brakes based on the user input commands.
8. A helicopter ground movement system according to claim 1 , wherein the helicopter user interface comprises a rotatable and tiltable user interface element, such as a puck, and wherein rotating the user interface element provides a steering command to the ground movement system and tilting the puck provides a speed command to the ground movement system.
9. A helicopter ground movement system according to claim 1 , comprising a mobile user interface provided on a mobile device operable to communicate the user input commands to the motors and steering actuators over a wireless interface, wherein the mobile user interface is provided in an application on a mobile computing device such as a tablet or smartphone.
10. A helicopter ground movement system according to claim 1 , further comprising:
control logic operable to limit the speed of movement of the helicopter on the ground, wherein the control logic is operatively linked to the wheel motors.
11. A helicopter ground movement system according to claim 1 , further comprising:
one or more proximity sensors arranged on the outside of the helicopter and operable to sense the proximity of external objects surrounding the helicopter and wherein the one or more proximity sensors are operable:
to communicate with the at least one user interface, wherein the at least one user interface is operable to provide a warning signal in the event the proximity sensor outputs indicate the helicopter comes to within a threshold distance of an external object; and
to communicate to the control arrangement proximity data indicative of the proximity of external objects, and wherein the control arrangement is operable to alter control signals that are based on the user input commands in dependence on the proximity data to avert a collision with an external object.
12. A helicopter ground movement system according to claim 1 , further comprising:
one or more cameras arranged around the helicopter and operable to send live video images of the helicopter surroundings to the at least one user interface.
13. A helicopter ground movement system according to claim 1 , further comprising:
one or more doors hingedly or slidably to the fuselage of the helicopter for each wheel, wherein the doors are arranged to enclose each wheel within the fuselage in a retracted position, and to open in order to allow the wheel to be deployed for landing.
14. A helicopter having a fuselage and rotor blades fixed to the top of the fuselage and comprising the ground movement system of claim 1 .
15. A ground movement method for a helicopter having a fuselage and rotor blades fixed to the top of the fuselage and at least three wheels secured below the fuselage, the ground movement method comprising:
receiving user input commands to control the speed and direction of travel of the helicopter via a user interface;
determining, based on the received user input commands, control signals for a first motor positioned in the wheel hub of a first of the at least three wheels and arranged to rotate the first wheel and control signals for a second motor positioned in the wheel hub of the second of the at least three wheels and arranged to rotate the second wheel; and
communicating the control signals to each of the first motor and the second motor;
wherein the user interface comprises a projecting user interface element movable between an up position and a down position, wherein in the up position the projecting user interface element protrudes from a surface of the user interface and is operable as at least one of a speed and steering controller for ground movement of the helicopter, wherein the projecting user interface element is tiltable to receive user input when in the up position but not when in the down position;
and wherein the step of receiving user input commands comprises receiving user input commands by tilting of the projecting user interface element when the user interface element is in the up position.
16. A ground movement method for a helicopter according to claim 15 , further comprising:
determining, based on the received user input commands, control signals for a first brake arranged to apply a braking force to the first wheel and control signals for a second brake arranged to apply a braking force to the second wheel; and
communicating the control signals to each of the first wheel and the second wheel.
17. A ground movement method for a helicopter according to claim 15 , wherein the user interface is removable from the helicopter, and wherein the method further comprises:
transmitting the user input commands over a wireless communication interface from the user interface to a control arrangement operable to determine the control signals and communicate the control signals to each of the first motor and the second motor, and where applicable to each of the first wheel and the second wheel.
18. A ground movement method for a helicopter according to claim 15 , further comprising:
receiving proximity data from one or more proximity sensors arranged on the outside of the helicopter, the proximity data being indicative of the proximity of one or more external objects to the helicopter;
determining from the proximity data within that the helicopter is within a threshold distance of an external object; and one or more of:
communicating the proximity data or data indicative of the proximity data to the at least one user interface; providing a warning signal on the user interface in dependence on the determination that the helicopter is within the threshold distance of an external object; and altering the determined control signals based on the proximity data prior to communicating the control signals to the first and second motors, and optionally to the first and second brakes.