Abstract: A method for controlling an aircraft when taxiing comprising the steps of: measuring an angle of rotation of an active side stick about a first axis and a second axis; receiving an aircraft signal representative of an actual state of the aircraft; generating a control signal based on at least one of: the aircraft signal and the angle of rotation of the active side stick about a first axis and a second axis; transmitting the control signal to the aircraft, whereby the control signal causes an action affecting the actual state of the aircraft; determining a required state of the aircraft; generating a user feedback signal based on at least one difference between the actual state and the required state; and carrying out a user feedback action based on the user feedback signal.

Abstract: A system and method of generating optimised aircraft flight trajectories on Flight Management Systems with limited computational power that takes into account developing operational conditions, air traffic constraints and aircraft performance in a timely manner on the flight management system that can allow tactical flight plan changes to be incorporated without unduly introducing operational or financial penalties to the operator. An example method involves parameterisation of optimal trajectories as functions of operational parameters thereby allowing computational systems to use such computed functions in the air to determine the optimal trajectory or flight profile required for the specific operating conditions quickly and accurately.

Abstract: A method and system for accurately calculating and implementing optimized airplane flight trajectories in the operational environment that requires the involvement and cooperation of various stakeholders that provide data from different agencies that are often physically located in different geographical locations, and executing the optimized trajectories in the operational environment.

Abstract: A method of recognizing at least one avionics system command from a voice command includes receiving a plurality of voice command definitions, each voice command definition identifying at least one avionics system command and identifying at least one voice command template that is mapped to the at least one avionics system command; receiving the voice command as raw speech; generating recognized speech by converting the raw speech into text; determining a voice command template that corresponds to the recognized speech; selecting a voice command definition, from among the plurality of voice command definitions, that identifies the determined voice command template; determining, as the at least one recognized avionics system command, the at least one avionics system command identified by the selected voice command definition; and providing the at least one recognized avionics system command to a avionics system for execution.

Abstract: A method and system is provided for the recovery of an aircraft energy upset in a time-constrained descent. The system includes a computational unit to assess a number of adjustments involving a combination of speed changes, aerodynamic brake deployment and track miles adjustments that alter the energy dissipation profile whilst allowing the aircraft to maintain a pre-determined time-of-arrival over an incoming waypoint along the original descent path.

Abstract: A method and system for interacting with the systems of an aircraft using touch screen technology that includes a human machine interface device for interacting with aircraft systems. The human machine interface including an input/display device configured to provide for navigating among graphical representations of a plurality of aircraft avionics systems via the common human machine interface; selecting an aircraft system via at least one of a touch gesture and a voice command input to the input/display device; inputting an instruction to the selected aircraft system; and outputting information via at least one of visual, aural, haptic and tactile channels.

Abstract: A system and method of generating optimised aircraft flight trajectories on Flight Management Systems with limited computational power that takes into account developing operational conditions, air traffic constraints and aircraft performance in a timely manner on the flight management system that can allow tactical flight plan changes to be incorporated without unduly introducing operational or financial penalties to the operator. An example method involves parameterisation of optimal trajectories as functions of operational parameters thereby allowing computational systems to use such computed functions in the air to determine the optimal trajectory or flight profile required for the specific operating conditions quickly and accurately.

Abstract: A method and system and tools for optimizing an aircraft flight trajectory that determine an advantageous flight profile that takes into account developing operational conditions, air traffic constraints and aircraft performance in a timely manner that can allow tactical flight plan changes to be incorporated without unduly introducing operational or financial penalties to the operator.

Abstract: A method and system for interacting with the systems of an aircraft using touch screen technology that includes a human machine interface device for interacting with aircraft systems. The human machine interface including an input/display device configured to provide for navigating among graphical representations of a plurality of aircraft avionics systems via the common human machine interface; selecting an aircraft system via at least one of a touch gesture and a voice command input to the input/display device; inputting an instruction to the selected aircraft system; and outputting information via at least one of visual, aural, haptic and tactile channels.

Abstract: A method and system is provided for the recovery of an aircraft energy upset in a time-constrained descent. The system includes a computational unit to assess a number of adjustments involving a combination of speed changes, aerodynamic brake deployment and track miles adjustments that alter the energy dissipation profile whilst allowing the aircraft to maintain a pre-determined time-of-arrival over an incoming waypoint along the original descent path.

Abstract: A method and system and tools for optimizing an aircraft flight trajectory that determine an advantageous flight profile that takes into account developing operational conditions, air traffic constraints and aircraft performance in a timely manner that can allow tactical flight plan changes to be incorporated without unduly introducing operational or financial penalties to the operator.

Abstract: A method and system for resolving existing and potential traffic conflicts that may occur during take-off and landing in aviation that includes means of monitoring movements on the runway, its approaches and environs to determine whether a conflict or potential conflict exists, means to resolve a conflict and to generate an output pertaining to this resolution.

Abstract: A method and system for resolving existing and potential traffic conflicts that may occur during take-off and landing in aviation that includes means of monitoring movements on the runway, its approaches and environs to determine whether a conflict or potential conflict exists, means to resolve a conflict and to generate an output pertaining to this resolution.

Abstract: A method and system for resolving existing and potential traffic conflicts that may occur during take-off and landing in aviation that includes means of monitoring movements on the runway, its approaches and environs to determine whether a conflict or potential conflict exists, means to resolve a conflict and to generate an output pertaining to this resolution.

Abstract: A system, method and display for monitoring the performance of an aircraft during the take-off maneuver that includes the steps of monitoring the progress of the take-off maneuver by acquiring data representative of the aircraft's motion at a plurality of points during the maneuver, generating a function that best fits the acquired data, and using the generated function to predict future progress of the maneuver.

Abstract: A system method and display for monitoring the performance of an aircraft during the take-off maneuver that includes the steps of monitoring the progress of the take-off maneuver by acquiring data representative of the aircraft's motion at a plurality of points during the maneuver generating a function that best fits the acquired data, and using the generated function to predict future progress of the maneuver.