Glide path indicator
Disclosed is a glide path indicator ( 2 ) comprising a light emitter ( 20 ) configured to emit a visible light signal that defines a glide path ( 14 ) for use by a pilot of an approaching aircraft ( 10 ), and a camera ( 22 ) configured to capture images of the approaching aircraft ( 10 ), the camera ( 22 ) being arranged such that at least part of the glide path ( 14 ) defined by the light emitter ( 20 ) is located within a field of view of the camera ( 22 ). The glide path indicator ( 2 ) may be mounted to a vehicle ( 4 ), for example, an aircraft carrier. The glide path indicator ( 2 ) may further comprise a stabilization module ( 26 ) configured to stabilize the light emitter ( 20 ) and the camera ( 22 ) so as to reduce or eliminate the effects of the vehicle's motion on the glide path ( 14 ) and the field of view of the camera ( 22 ).
1. A glide path indicator configured to be mounted on a vehicle, said glide path indicator comprising:
a light emitter configured to emit a visible light signal that defines a glide path for use by a pilot of an approaching aircraft;
a camera configured to capture images of the approaching aircraft, the camera being arranged such that at least part of the glide path defined by the light emitter is located within a field of view of the camera; and
a common stabilisation module configured
to stabilise the light emitter so as to reduce or eliminate the effects of the vehicle's motion on the glide path, and
to stabilise the camera so as to reduce or eliminate the effects of the vehicle's motion on the camera's field of view.
2. A glide path indicator according to claim 1 , wherein the camera is arranged such that the glide path defined by the light emitter is wholly located within the field of view of the camera.
3. A glide path indicator according to claim 1 , wherein the vehicle is a ship.
4. A glide path indicator according to claim 1 , wherein the light emitter and the camera are coupled together such that the position and orientation of the camera with respect to the light emitter are fixed.
5. A glide path indicator according to claim 1 and further comprising means for preventing or opposing light emitted by the light emitter from being received by the camera.
6. A glide path indicator according to claim 5 , wherein the means for preventing or opposing light emitted by the light emitter from being received by the camera comprises means selected from the group consisting of:
an opaque screen located between the light emitter and the camera;
a filter configured to filter light being received by the camera, the filter being configured to block only light having a wavelength equal to that of the light emitted by the light emitter; and
a switch operable to switch the glide path indicator between a first state and a second state, the first state being a state in which the light emitter emits light and the camera does not capture images, and the second state being a state in which the light emitter does not emit light and the camera captures images.
7. A glide path indicator according to claim 1 and further comprising a transmitter configured to transmit, to an entity remote from the glide path indicator, the images captured by the camera.
8. A glide path indicator according to claim 1 , wherein the light emitter is a pulsating visual approach slope indicator.
9. A vehicle comprising a glide path indicator, the glide path indicator being in accordance with claim 1 .
10. A vehicle according to claim 9 , wherein the vehicle is a ship.
11. A method of assessing a descent profile of an aircraft during a landing operation, the method comprising:
providing a glide path indicator configured to be mounted on a vehicle, the glide path indicator comprising:
a light emitter configured to emit a visible light signal that defines a glide path for use by a pilot of the aircraft during the landing operation; and
a camera configured to capture images of the aircraft during the landing operation, the camera being arranged such that at least part of the glide path defined by the light emitter is located within a field of view of the camera;
emitting, by the light emitter, a visible light signal so as to define the glide path for use by the pilot of the aircraft;
imaging, by the camera, the aircraft; and
using the images of the aircraft, determining an assessment of a descent profile of the aircraft
a common stabilisation module configured
to stabilise the light emitter so as to reduce or eliminate the effects of the vehicle's motion on the glide path, and
to stabilise the camera so as to reduce or eliminate the effects of the vehicle's motion on the camera's field of view.
12. A method according to claim 11 , the method further comprising:
using the determined assessment, determining an action that, if performed by the aircraft, would establish the aircraft on the glide path; and
controlling the aircraft to perform the determined action.