Abstract: An aircraft environmental control system (4) for controlling a temperature of a fluid, the control system comprising: a temperature sensor (30) configured to measure a temperature of the fluid and generate a signal indicative of that temperature; a control signal generator (52) configured to, using control laws (78) and the first signal, generate a control signal for controlling the temperature of the fluid; a memory (56) for storing performance data; a transmitter (60) configured to transmit, from the aircraft environmental control system (4), the performance data; a receiver (60) configured to receive, responsive to transmitting the performance data, update information; and an update module (58) configured to, using the update information, update the control laws (78).

Abstract: Disclosed is a method of managing a plurality of individual nodes in a communication network, wherein one of the plurality of nodes is operating in the vicinity of a jurisdictional boundary and is expected to cross the boundary, comprising the steps of: a network controller retrieving, from a spectrum access database, operating parameter information for the node expected to cross the boundary, wherein the operating parameter information comprises operating parameters relating to a present location of the node and an expected future location; the network controller determining operating parameter information for use by the node, whereby the operating parameter information causes the node to comply with relevant regulations in the present and expected future location; and the network controller transmitting the determined operating parameter information to the node.

Abstract: Apparatus for management of communications resources of a moving platform comprising a communications system configured to effect wireless data communication between the moving platform and a recipient node, the communications resources comprising a plurality of wireless communications links for facilitating the wireless data communication and a plurality of antennas associated therewith, the apparatus comprising an antenna analysis and selection module residing with the communications system and configured to: identify a communications requirement between the moving platform and a recipient node; receive attribute data representative of movement of the platform, the attribute data including platform movement data comprising future known movement of the moving platform and/or future predicted movement of the moving platform and/or the recipient node; determine, using the attribute data, suitability of each of a plurality of antennas and/or portions of aperture antenna for data transmission from the moving

Abstract: Apparatus for on-board management of communications in a mobile node comprising a communications system configured to effect wireless data communication between the mobile node and another node by means of at least one supported wireless communications link, wherein the apparatus comprises a node manoeuvre planning module and a dynamic route planner; the node manoeuvre planning module being configured to: identify that a wireless communications link associated with the mobile node (i) has been lost, degraded or is otherwise not optimal, and/or (ii) would violate an emissions control restriction; define a desired wireless communications link between the mobile node and the other node to (i) support wireless communications therebetween, and/or (ii) comply with the emissions control restriction; determine an attitude and/or position of the mobile node with respect to the other node required to support the desired wireless communications link; derive a node manoeuvre plan including data representative of the d

Abstract: Disclosed is an ATC Radar and a method of operating an ATC Radar, including the steps of: receiving In-phase (I) and Quadrature (Q) signals; creating first and second complex clutter maps using the I and Q signals; wherein the first map comprises data which is dynamically updated on a per-scan basis and the second map comprises data indicative of a static environment with no targets; subtracting data from the second map from the received I and Q signals to mitigate the effects of static objects in the environment, to yield compensated I and Q data; and using the compensated I and Q data for target detection and/or tracking.

Abstract: A system/method of diagnosing combinations of failures in a system includes receiving symptom data (116) including information relating to observed or detected symptoms in a system. The system/method generates (D4a, D4b, D5) failure data (118) including information relating to at least one most probable failures in the system based on the symptom data, and processes (D9) the failure data and the symptom data using an L-best inference (e.g. a Ranked Algorithm (RA)) technique in order to generate failure set data (120), the failure set data including information relating to at least one most probable combination of the failures that explain the symptoms.

Abstract: A driver circuit for an LED display for switching a light-emitting diode (LED) between a non-luminous state and a luminous state for producing light for a display, the driver circuit comprising an LED, a drive current controller (10) arranged to selectively open and close a drive current flow path (8) through the LED (2) thereby selectively to switch the LED between a non-luminous state and a luminous state, a charge injector unit (13) for inputting charge into the LED to store said charge within the LED via the junction capacitance (3) thereof, a control unit (12) arranged to control the charge injector unit to input said charge into the LED concurrently with the opening of the drive current flow path.

Abstract: An aircraft (101) is provided with a single centrally located inceptor (110) for controlling pitch and roll of the aircraft. The inceptor (110) is provided with a double grip (11, 112) so that it may be comfortably operated by either a pilot or a co-pilot. A central location for the inceptor ensures that its motion and position is visible to both pilot and co-pilot. Not only is this a benefit from a safety point of view but also during pilot training. Alternatively, two inceptors (411, 412) are provided in the centre console (406) adjacent to one another for operation respectively by the pilot and co-pilot and may be mechanically linked. Optionally, the aircraft may be provided with outboard throttle quadrants (117, 118) for operation respectively by the co-pilot and pilot. The outboard throttle quadrants may be mechanically linked together.

Abstract: A waveguide structure for a head up display in which a reflective output coupling structure is formed of a separate, but connected, component to a main waveguide. In a method of manufacture for such a waveguide the output coupling structure may be formed by depositing a material on a main waveguide, impressing the reflective structure into that material, and curing the material.

Abstract: A waveguide structure for a head up display in which a reflective output coupling structure is formed of a separate, but connected, component to a main waveguide. Light is coupled from the main waveguide to the output coupling structure by evanescent wave coupling. In a method of manufacture for such a waveguide the output coupling structure is attached to the main waveguide using an optical feedback technique.

Abstract: Disclosed is a method and apparatus for detecting cloud features. The method comprises: obtaining image data (e.g. using a camera), the image data defining a plurality of pixels and, for each pixel, a respective luminance value; defining one or more intervals for the luminance values of the pixels; partitioning the image data into one or more image segments (502-508), each respective image segment (502-508) containing pixels having a luminance value in a respective interval; and classifying, as a cloud feature, each image segment (502-508) containing pixels having luminance value greater than or equal to a threshold luminance value (LT).

Abstract: A method and apparatus for generating, in an aircraft in flight, a feasibility display indicative of the feasibility of a weapon, the method comprising: providing a performance envelope for the weapon; determining, using the performance envelope, configuration data for configuring a generic algorithm; uploading the configuration data to the aircraft; generating feasibility data N indicative of the feasibility of a weapon carried on the aircraft successfully engaging a target and/or the feasibility of a weapon carried on the target successfully engaging the aircraft; determining, on board the aircraft, using the same generic algorithm and the uploaded configuration data, one or more test criteria; performing, on board the aircraft, an assessment process including determining whether or not the feasibility data satisfies the one or more test criteria; and, based the assessment, using the feasibility data, generating the feasibility display.

Abstract: An optical waveguide device for use in a head up display. The waveguide device provides pupil expansion in two dimensions. The waveguide device comprise a primary waveguide and a secondary waveguide, the secondary waveguide being positioned on a face of the primary waveguide. The secondary waveguide has a diffraction grating on a face opposite to the face which contacts the primary waveguide. The diffraction grating diffracts light into more than diffraction order. Rays diffracted into a non-zero order are trapped in the secondary waveguide by total internal reflection.

Abstract: A mixed reality control apparatus for a system having at least one remote data source requiring at least one physical control input, the apparatus comprising a headset for placing over a user's eyes, in use, the headset including a screen, the apparatus further including a processor configured to receive data from the at least one remote data source and display the data on the screen within a three-dimensional virtual environment, and image capture means for capturing images of the real world environment in the vicinity of the user, the processor being further configured to: blend at least portions or objects of the images of the real world environment into the three-dimensional virtual environment to create a mixed reality environment, including the data, to be displayed on the screen; and generate a virtual representation of the at least one physical control input and blend the virtual representation into the mixed reality environment at a selected location, and generate a marker representative of the selec

Abstract: Disclosed are methods and apparatus for selectively sintering particulate material, the method comprising: providing a layer (6) of particulate material; providing an amount of a radiation absorbent material over a selected surface portion of the layer (6) of particulate material; providing an amount of a material that comprises a plurality of electrically conductive elements (20) over at least part of the selected surface portion of the layer (6) of particulate material; and providing radiation (8) across the selected surface portion of the layer of particulate material so as to sinter a portion of the material of the layer (6) including causing the plurality of electrically conductive elements (20) to become embedded in the sintered portion of material.

Abstract: Methods and systems for producing data describing target measurements using a processor (102) in a system (100) having at least one on-board sensor (106) on a vehicle. The method includes obtaining data from an on-board sensor (106), obtaining data from a sensor (108) off-board the vehicle, approximating (312) a target alignment error between the on-board and off-board sensor data, receiving target alignment error data in respect of at least one other sensor set comprising at least two sensors, estimating (316) a bias using the received target alignment error data and correcting the approximated target alignment error using the bias, and performing (320) a data fusion process on the obtained off-board sensor data and the obtained on-board sensor data using the approximated target alignment error to produce target measurement data.

Abstract: A method and system configured to evaluate near range communications quality in an environment. Data describing an environment is obtained from at least one data source (202). The data describing the environment is processed (204) to generate a ground-plane data set (206) describing a ground-plane of the environment, and a 3D object data set (206) describing 3D objects in the environment. These data are used to compute (208) a propagation path between a first location and a second location in the environment, and a near range communications quality characteristic of the propagation path is computed (210).

Abstract: Disclosed is a method and apparatus for determining a route for a vehicle (2). The method comprises generating, by a processor (12), a grid (16) by specifying a start node (18), specifying one or more movement operations performable by the vehicle (2), and iteratively adding edges and further nodes (20-24) to the grid (16), each edge corresponding to a respective movement operation and each further node corresponding to a location for the vehicle (2). The one or more processors (12) then select a path through the grid (16) from a first node of the grid to a second node of the grid. The first node corresponds to a first location (A) for the vehicle (2) and the second node corresponds to a second location (B) for the vehicle (2). Thus, a route for the vehicle (2) from the first location (A) to the second location (B) is determined.

Abstract: A vehicle (100) comprising: an engine (102); a system for starting the engine (102); a fault detection module (120); an electrical power source (110); and a controller (116, 122). The controller (116, 122) is configured to, responsive to the fault detection module (120) detecting a fault occurring with the engine (102): determine a window in which to attempt to start the engine (102); control the electrical power source (110) to provide electrical power to the system for starting the engine (102); and control the system for starting the engine (102) to attempt to start the engine (102) using the supplied electrical power only during the determined window.

Abstract: An aircraft environmental control system (4) for controlling a temperature of a fluid, the control system (4) comprising: a temperature sensor (30) configured to measure a temperature of the fluid and to generate a first signal, the first signal being indicative of the measured temperature; a control signal generator (52) configured to, dependent upon the first signal, generate a control signal for controlling the temperature of the fluid; and one or more processors (64) configured to, responsive to determining that the measured temperature is less than or equal to a pre-determined threshold value (e.g. 0° C.), increase a gain of the control signal generator (52).