Abstract: A method and system method for estimating fatigue damage in a structure obtains fatigue damage data collected using at least one sensor associated with the structure during at least one test operation and also obtains structure use parameter data collected during the at least one test operation. The obtained fatigue data and the obtained use parameter data are used to compute coefficients of at least one generic polynomial function that outputs a fatigue damage value based on inputs representing use parameter data. The at least one generic polynomial function is used to output an estimated fatigue damage value based on inputs representing use parameter data collected during use of the structure.

Abstract: A method and system method for estimating fatigue damage in a structure obtains fatigue damage data collected using at least one sensor associated with the structure during at least one test operation and also obtains structure use parameter data collected during the at least one test operation. The obtained fatigue data and the obtained use parameter data are used to compute coefficients of at least one generic polynomial function that outputs a fatigue damage value based on inputs representing use parameter data. The at least one generic polynomial function is used to output an estimated fatigue damage value based on inputs representing use parameter data collected during use of the structure.

Abstract: An emissions management module for a mission management system of a moving platform, said emissions management module being configured to: —obtain attribute data representative of (i) prevailing emissions control parameters in the form of an emissions control region defined by the relative locations of said platform and another node; and (ii) a direction of said emissions control region with respect to said platform; —generate, using said attribute data, an emissions plan that complies with restrictions defined by said emissions control parameters, and includes at least an emissions limit defining: a) a maximum transmission power permitted to be utilised by an on-board antenna or portion of aperture antenna in a specified direction relative to said moving platform; and/or b) permissible antenna waveforms and/or a specified maximum emissions duration in said specified direction relative to said moving platform; and/or c) permitted or restricted usage of on-board sensors in a specified direction relative to sai

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 a system and method for generating, in an aircraft (1) in flight, a display indicative of the feasibility of a weapon carried on the aircraft (1) successfully engaging a determined target (5, T) and/or the feasibility of a weapon carried on the target (5, T) successfully engaging the aircraft (1). The method comprises: using a performance envelope of the weapon and performance envelope(s) for one or more different types of aircraft (1), determining a further performance envelope specifying the performance of the weapon when carried by any of the different aircraft (1) types; determining coefficients for a generic polynomial that fit the generic polynomial to the further performance envelope; uploading, to the aircraft (1), the generated coefficients; and, on the aircraft (1), reconstructing the further performance envelope and generating the feasibility display.

Abstract: Disclosed is a system and method for generating, in an aircraft (1) in flight, a display indicative of the feasibility of a weapon carried on the aircraft (1) successfully engaging a determined target (5, T) and/or the feasibility of a weapon carried on the target (5, T) successfully engaging the aircraft (1). The method comprises: using a performance envelope of the weapon and performance envelope(s) for one or more different types of aircraft (1), determining a further performance envelope specifying the performance of the weapon when carried by any of the different aircraft (1) types; determining coefficients for a generic polynomial that fit the generic polynomial to the further performance envelope; uploading, to the aircraft (1), the generated coefficients; and, on the aircraft (1), reconstructing the further performance envelope and generating the feasibility display.

Abstract: Systems and methods of integrating weapons systems with the aircraft systems of an aircraft carrying the weapon so as to generate on the aircraft in flight a display indicative of the weapon successfully engaging a target are disclosed. The system can include a ground station for generating a database describing the weapon performance envelope, a generator for creating coefficients characteristic of that performance envelope using a generic algorithm and an uploader for uploading the coefficients to the aircraft, and a reconstructor on the aircraft containing the same generic algorithm and adapted to select the coefficients for the algorithm according to the aircraft and target conditions in order to generate the feasibility display, wherein the algorithm is generic to both air to ground and air to air weapons.

Abstract: Systems and methods of integrating weapons systems with the aircraft systems of an aircraft carrying the weapon so as to generate on the aircraft in flight a display indicative of the weapon successfully engaging a target are disclosed. The system can include a ground station for generating a database describing the weapon performance envelope, a generator for creating coefficients characteristic of that performance envelope using a generic algorithm and an uploader for uploading the coefficients to the aircraft, and a reconstructor on the aircraft containing the same generic algorithm and adapted to select the coefficients for the algorithm according to the aircraft and target conditions in order to generate the feasibility display, wherein the algorithm is generic to both air to ground and air to air weapons.