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8447442 |
Method for assisting in rejoining a vertical descent trajectory and associated device
A method is provided for assisting in rejoining a vertical descent trajectory that an aircraft is assumed to have to follow, using a flight management system FMS embedded onboard the aircraft, and...
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8447441 |
Aircraft power management system
A method and associated system for managing power within an aircraft electrical system, the aircraft having a generator driven by a gas turbine engine for the supply of electrical power to the...
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8447443 |
Systems and methods for peak-seeking control
A computerized system and method for peak-seeking-control that uses a unique Kalman filter design to optimize a control loop, in real time, to either maximize or minimize a performance function of...
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8442704 |
System and method for computing an equi-distance point (EDP) for aircrafts
A method for dynamically computing an equi-distance point (EDP) for an aircraft includes receiving at least two reference points for landing the aircraft upon an occurrence of an emergency,...
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8442705 |
Method and device for determining aerodynamic characteristics of an aircraft
The present invention provides a device and method for determining aerodynamic characteristics of an aircraft, in particular a pitch moment coefficient at an ascending force of the aircraft without...
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8442751 |
Onboard electronic distribution system
A computer implemented method, apparatus, and computer program product for transferring information with an aircraft. A connection is established between an onboard electronic distribution system...
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8442707 |
Implementing continuous descent approaches for maximum predictability in aircraft
The present invention relates to continuous descent approaches that ensure the greatest certainty in arrival time. The continuous descent approach is flown by maintaining an aerodynamic flight path...
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8442702 |
Fault diagnosis device and method for optimizing maintenance measures in technical systems
The present invention provides a fault diagnosis device for optimizing maintenance measures in a system, in particular a flying object. The diagnosis device has a storage unit for storing diagnosis...
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8442701 |
Dynamic roll angle stall protection for an aircraft
A method, apparatus, and computer program product are present for operating an aircraft. A roll angle limit is identified using a load factor selected to allow a lateral maneuvering capability of...
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8442703 |
Turning-stabilized estimation of the attitude angles of an aircraft
The present invention relates to estimating the attitude angles of an aircraft (1). The estimated attitude angles are generated by a device (9) that performs algorithmic integration on inertial...
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8437888 |
Distributed architecture for all radionavigation aids
The present invention relates to a distributed architecture for all aerial navigation aids. So that this architecture makes it possible to reduce the weight and/or the bulk of the cables linking...
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8437893 |
Determining current meteorological conditions specific to an aircraft
A method of providing meteorological data for aeronautical use. The method includes collecting data from a plurality of data sources, processing the data to determine current meteorological...
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8437890 |
Integrated framework for vehicle operator assistance based on a trajectory prediction and threat assessment
Various types and levels of operator assistance are performed within a unified, configurable framework. A model of the device with a model of the environment and the current state of the device and...
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8437956 |
Unmanned aerial system position reporting system and related methods
Methods of communicating the location of an unmanned aerial system (UAS). Implementations of the method may include receiving position data for a UAS with an air traffic control reporting system...
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8437887 |
Method for optimizing a fuel consumption of an aircraft during the flight thereof
The invention relates to a method for optimizing the fuel consumption of an aircraft during flight. At a given point of the flight, a fuel excess (EXTRA) is determined relative to the statutory...
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8437889 |
Test equipment for testing an additional center tank (ACT) system of an aircraft
The present invention provides test equipment for testing an additional center tank (ACT) system of an aircraft. The ACT system comprising control means configured to perform functions of an...
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8436283 |
System and method for guiding and controlling a missile using high order sliding mode control
Higher Order Sliding Mode (HOSM) control techniques are applied to the Guidance Control (G&C) of interceptor missile in which velocity may be steered by combination of main thrust, aerodynamic lift...
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8437894 |
Method and system for improving the performance of an aircraft upon take off
A method and system for improving aircraft performances during take-off is described. The system (1) can include means (4, 6, 7) for determining an optimised take-off position of the control...
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8433457 |
Environmental condition detecting system using geospatial images and associated methods
An environmental condition detecting system may include an image processor cooperating with a database for generating a reference geospatial image corresponding to the collected geospatial image, a...
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8433458 |
Method and device for assisting in the preparation and management of missions in an aircraft
Aiding preparation and management of aircraft missions includes receiving digital data including avionic type data and open-world type data and comparing the digital data with a set of stored data....
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8433475 |
Maintenance computer system for an aircraft
A maintenance computer system for an aircraft, including a network partitioned into a secured avionics zone and an open zone. The system includes a first software module accommodated in the...
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8433506 |
Weather data selection relative to an aircraft trajectory
A method of providing weather information for an aircraft trajectory to a flight management system (FMS) includes selecting a unique subset of temperature data points from weather data points along...
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8433459 |
Aircraft guidance system for assisting in airport navigation
An aircraft guidance system for assisting in airport navigation includes: at least one airport database comprising topology data of an airport, called airport DB; at least one configuration...
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8433460 |
Onboard sensor suite for determining projectile velocity
An onboard sensor suite generally includes two main components: a proximity sensor suite for measuring the projectile muzzle velocity; and a pressure sensor suite for measuring the projectile...
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8428872 |
System and method for entry of taxi route on control display unit
A system and method is provided for receiving and displaying a taxiway navigation route on a control display unit having at least one entry field and a plurality of display lines. A plurality of...
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8423331 |
Method for optimisation of an avionics platform
A method for optimization of the avionics platform of an aircraft, intended to implement a set of avionics functions. The association between the platform's functional architecture elements...
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8423207 |
Integrated approach navigation system, method, and computer program product
Systems, computer program products, and methods for displaying navigation performance based flight path deviation information during the final approach segment to a runway and during landing of...
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8423204 |
Electronic device and method for controlling unmanned aerial vehicle using the same
A method for controlling an unmanned aerial vehicle (UAV) using an electronic device obtains movement data of an object on a display screen of the electronic device, and converts the movement data...
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8423009 |
Automated delivery of flight data to aircraft cockpit devices
Flight data and information update files such as electronic charts used by aircraft cockpit devices are automatically installed by a secure, wireless delivery system. A service provider downloads...
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8423206 |
Variable maximum commandable roll rate for directional control during engine-out rolling maneuver
A system and a method for varying a maximum roll rate command for ensuring sufficient directional control during an engine-out rolling maneuver of a multi-engine aircraft. For a multi-engine...
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8415596 |
Method and apparatus for determining a location of a flying target
A method for determining a location of a flying target included identifying and measuring the target by at least two seeker systems disposed at a distance from one another. The position of the...
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8417410 |
Operations support systems and methods with power management
A power management system includes a data fusion unit configured to receive first health indicators from an engine diagnostics module and second health indicators from a power assurance module. The...
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8417397 |
Vertical profile display with variable display boundaries
A display system includes instrumentation configured to obtain aircraft data comprising current flight status data of the host aircraft and current flight status data of neighboring aircraft...
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8417396 |
Air traffic control method
A method of operating an air traffic control system may include receiving, by a control system, an instruction from a control system user. The method may further include providing, by the control...
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8416152 |
Method and system for operating a near-to-eye display
Methods and systems for operating a vehicular near-to-eye (NTE) display screen operable within an operational range limit are provided. An image is rendering on the NTE display screen within a...
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8417395 |
Hierarchical closed-loop flow control system for aircraft, missiles and munitions
The present invention relates to a missile or aircraft with a hierarchical, modular, closed-loop flow control system and more particularly to aircraft or missile with a flow control system for...
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8412389 |
Integrity monitoring of inertial reference unit
Systems, methods, and machine-executable programming products adapted for the control of aircraft or other vehicles by receiving from at least one Inertial Reference System (IRS), including a...
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8412388 |
Assisted piloting method and device for an aircraft for use in the event of a first limit indicator breaking down
An assisted piloting method for an aircraft having at least two engines (2, 3) includes monitoring a set of parameters (Ng, T4, Tq) of the engines. A first limit indicator (10) displays information...
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8406936 |
Modular battery network system with life-optimal power management
A system and methods for life optimal power management of a distributed or centralized battery network system for use in aircraft functions and subsystems are disclosed. The method determines power...
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8406939 |
Systems and methods for RTA control of multi-segment flight plans with smooth transitions
Methods, systems and device are provided for smoothing a required time of arrival (RTA) speed transition for an aircraft in a multi-segmented speed profile including at least one preceding region...
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8401860 |
Voice-activated command and control for remotely controlled model vehicles
A voice-activated command and control system for remotely-controlled vehicles includes a voice-activated control module, a microphone, and a verbal or visual feedback indicator such as a speaker....
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8401716 |
Flight control systems
A system and method for a controlling an aircraft with flight control surfaces that are controlled both manually and by a computing device is disclosed. The present invention improves overall...
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8400347 |
Device and method for monitoring the location of aircraft on the ground
The invention relates to a monitoring device and method allowing surveillance of an aircraft in relation to aircraft and/or craft on an airport displacement zone. The invention is a system...
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8401790 |
Computing-time-efficient route determination along several preset path points with given connecting routes in-between
A process for determining a route along more than two mutually consecutive preset path points with given connecting routes in-between. In this case, a plurality of connecting routes is given...
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8401717 |
Actuator control reducing the level of vibration of an associated flexible structure
The aim of the method of controlling at least one mechanical system exhibiting at least one flexible structure element and at least one actuator or group of actuators is to reduce the level of...
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8401773 |
Air traffic control
An air traffic control system, for use by a human controller controlling a plurality of aircraft held vertically separated in a stack above a minimum stack level, the system comprising at least one...
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8401718 |
Method of and system for maintaining operating performance of a transparency
Repair or replacement of a transparency mounted in body of a vehicle, e.g. an aircraft when one or more properties of the transparency is (are) operating outside of an acceptable limit(s) is...
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8396614 |
Graphical depiction of four dimensional trajectory based operation flight plans
The different advantageous embodiments provide a system comprising a user interface and a computer. The user interface comprises a display. The computer is configured to display information about...
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8396613 |
Method and apparatus for providing power in an aircraft to one or more aircraft systems
A method and apparatus is disclosed in which an aircraft system such as the landing gear system or braking system is operated at least partially under power provided by a generator driven by the...
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8396612 |
Avionic system and architecture with integrated power management
An avionic system includes computers (11a, . . . , 1n, 12a, . . . 12n, 13a . . . 13n) of the generic computer type that can be adapted by software programming to avionic functions for which at...
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