Match Document Document Title
US20140309818 RAM AIR TURBINE AUTODEPLOYMENT LOGIC  
A ram air turbine deployment module includes a normal power module that determines if normal power from an aircraft is available, an air-ground module that determines if the aircraft is off the...
US20130325212 AERIAL VEHICLE WITH MISSION DURATION CAPABILITY DETERMINATION  
An aerial vehicle can include oil sensors connected to a lubrication system and a computer connected to the oil sensors. The computer can be programmed to determine mission duration for the...
US20120239227 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...
US20120043414 CONTROL OPTIMIZATION METHOD FOR HELICOPTERS CARRYING SUSPENDED LOADS  
The control optimization method for helicopters carrying suspended loads during hover flight utilizes a controller based on time-delayed feedback of the load swing angles. The controller outputs...
US20140039729 CUBESAT SYSTEM, METHOD AND APPARATUS  
A satellite system includes a chassis, an avionics package included within an upper portion of the chassis. The avionics package includes a main system board, a payload interface board, at least...
US20140114505 Yaw Damping System And Method For Aircraft  
An alternative system for damping the dutch roll mode in an aircraft is provided using roll control surfaces. Classical yaw dampers for the dutch roll mode utilize the yaw control surfaces such as...
US20130226374 Yaw Damping System And Method For Aircraft  
An alternative system for damping the dutch roll mode in an aircraft is provided using roll control surfaces. Classical yaw dampers for the dutch roll mode utilize the yaw control surfaces such as...
US20090005917 System and method of carbon monoxide and fire detection and protection  
A carbon monoxide and fire detection system and method are provided for vehicles, particularly light aircraft, which includes CO and smoke/heat detectors located in or near the pilot cabin that,...
US20130240673 ENABLING MULTIPLE AUTONOMOUS CARGO DELIVERIES IN A SINGLE MISSION  
Some embodiments of the invention provide methods and apparatus enabling multiple unmanned cargo deliveries in a single mission. An assembly having multiple hooks may be coupled to an unmanned...
US20120323410 FATIGUE MANAGEMENT SYSTEM  
A fatigue management system for determining the individual life of an aircraft, particularly the individual life of components of a helicopter, by means of an on board virtual load sensor and a...
US20150120094 UNMANNED AERIAL VEHICLE DELIVERY SYSTEM  
This disclosure describes an unmanned aerial vehicle (“UAV”) configured to autonomously deliver items of inventory to various destinations. The UAV may receive inventory information and a...
US20130035809 METHOD AND SYSTEM FOR DETERMINING FLIGHT PARAMETERS OF AN AIRCRAFT  
According to the invention, the system for determining, in real time, flight parameters of an aircraft, in the course of a flight of the latter, comprises an extended Kalman filter (10) which is...
US20150081141 METHOD AND SYSTEM FOR COORDINATING REMOVAL OF CONTAMINATION FROM SURFACE OF AIRCRAFT  
A method for coordinating contamination removal on a surface of an aircraft, comprising receiving an electronic contamination removal request, determining location for contamination removal...
US20110121127 POWER PLANT, A HELICOPTER INCLUDING SUCH A POWER PLANT, AND A METHOD IMPLEMENTED BY SAID POWER PLANT  
The present invention relates to a power plant (10) having a single engine (13) together with both a main gearbox (MGB) suitable for driving the rotary wing (3) of a helicopter (1) and a tail...
US20110313598 METHOD AND SYSTEM FOR DYNAMICALLY MANAGING A FLIGHT PROCEDURE OF AN AIRCRAFT FLIGHT PLAN  
A method of managing a flight procedure of an aircraft flight plan, which has at least one segment, includes a step in which an additional attribute of the segment representative of a compulsory...
US20090138140 VEHICULAR LINEAR SENSOR SYSTEM  
Vehicular sensor systems are provided. The vehicular sensor systems includes a support, first, second, and third sensors, and a support actuator. The first sensor is coupled to the support and...
US20120215387 TECHNIQUE FOR PROVIDING MULTIPLE UNDO AND REDO OPERATIONS FOR FLIGHT MANAGEMENT SYSTEMS  
A technique for providing multiple undo and redo operations for flight management systems is disclosed. In one embodiment, in a method of providing multiple undo and redo operations for a flight...
US20100308154 METHOD OF CONTROLLING A HYBRID HELICOPTER IN YAW, AND A HYBRID HELICOPTER PROVIDED WITH A YAW CONTROL DEVICE SUITABLE FOR IMPLEMENTING SAID METHOD  
A method of controlling the yaw attitude of a hybrid helicopter including a fuselage and an additional lift surface provided with first and second half-wings extending from either side of the...
US20150148999 MISSION MANAGEMENT SYSTEM OF AN AIRCRAFT  
A mission management system to manage both ground and flight phases of a mission of an aircraft is proposed. The mission management system may be implemented in flight management system...
US20130175387 Altitude Control Via Rotation of Balloon to Adjust Balloon Density  
A balloon that includes an envelope with a gas contained within the envelope, as well as a payload connected to the envelope wherein the envelope has a first portion that has a first absorptive or...
US20130325216 SYSTEM AND METHOD FOR AUTHORIZING STOPPAGE OF PILOTING TASKS  
A system and method for authorizing stoppage of piloting tasks performed by at least one pilot of an aircraft equipped with automatic piloting means is disclosed. A duration for which the stoppage...
US20130079956 METHOD OF REGULATING THE PROPULSIVE SPEED OF A HYBRID HELICOPTER  
A method of regulating the propulsion speed of a hybrid helicopter. In application of a correction process for protecting the hybrid helicopter, piloting orders generated by a manual control...
US20130158750 Energy Management On Board an Aircraft  
Energy management on board an aircraft includes: a plurality of thermal and electrical energy sources, a plurality of loads which are capable of being supplied with power by the various energy...
US20130282205 STANDBY INSTRUMENT FOR AN AIRCRAFT, THE INSTRUMENT PROVIDING FLIGHT INFORMATION, POWER MARGIN INFORMATION, AND ASSISTANCE IN PILOTING  
A standby instrument (10) for an aircraft, the instrument comprising at least one inertial sensor (1), at least one pressure sensor (2), calculation means (3) connected to said inertial and...
US20110160936 METHOD AND DEVICE FOR ACCESSING THE DOCUMENTATION OF AN AIRCRAFT ACCORDING TO ALARMS GENERATED THEREIN  
The invention in particular has as an object a method and a device for accessing the documentation of an aircraft according to alarms generated therein, the documentation comprising at least one...
US20140365037 FAULT TOLERANT LATERAL WAYPOINT SEQUENCING SYSTEM AND METHOD  
Fault-tolerant lateral waypoint sequencing is provided for a system that includes at least a first flight management computer and a second flight management computer. A processing operation...
US20140032016 ADVANCED COOPERATIVE DEFENSIVE MILITARY TACTICS, ARMOR, AND SYSTEMS  
This invention provides impact detection and vehicle cooperation to achieve particular goals and determine particular threat levels. For example, an impact/penetration sensing device may be...
US20150142222 APPARATUS AND METHOD FOR TRACING FLIGHT PLAN STATUS  
An apparatus and a method for tracing a flight plan status are disclosed. The apparatus for tracing a flight plan status includes: a flight plan structure generation unit configured to generate a...
US20140027131 WILDFIRE ARREST AND PREVENTION SYSTEM  
An apparatus, operations controller and methods for controlling unmanned aerial vehicles for detection, prevention and suppression of fires in a designated zone are presented. Monitored...
US20140012436 METHOD FOR AIDING NAVIGATION MAKING IT POSSIBLE TO MANAGE A VERTICAL CONSTRAINT IN AN ANTICIPATED MANNER  
A method for aiding navigation is provided, implemented in a flight management system, for the construction of a vertical trajectory of an aircraft following a predetermined lateral trajectory...
US20100324755 Method and system for resolving traffic conflicts in take-off and landing  
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...
US20140214244 ELECTRONIC BOARD FOR AVIONICS EQUIPMENT COMPRISING VIBRATION DAMPING MEANS BETWEEN ITS REINFORCING SURROUND AND ITS RETENTION MEANS  
An electronic board for avionics equipment, the board comprising a printed circuit, a reinforcing surround and board retention means. In order to improve the vibration resistance of the board, the...
US20150134150 AIRCRAFT AVOIDANCE METHOD AND DRONE PROVIDED WITH A SYSTEM FOR IMPLEMENTING SAID METHOD  
A method enabling an aerial drone not having a TCAS system to avoid an intruder aircraft, the method including the steps of acquiring the position of the intruder aircraft in order to determine...
US20100312421 DEVICE FOR ASSISTING IN PILOTING A HYBRID HELICOPTER, A HYBRID HELICOPTER PROVIDED WITH SUCH A DEVICE, AND A METHOD IMPLEMENTED BY SAID DEVICE  
A piloting assistance device for a hybrid helicopter is provided with a rotary wing, two half-wings (8′, 8″) provided respectively with first and second propellers (6′, 6″), and an engine...
US20130013131 METHOD AND APPARATUS FOR PARAFOIL GUIDANCE THAT ACCOUNTS FOR GROUND WINDS  
A method is described that involves determining a higher altitude wind. The method further includes determining a wind model with the higher altitude wind. The wind model includes a linear or...
US20100327124 METHOD AND DEVICE FOR LATERALLY TRIMMING AN AIRPLANE DURING A FLIGHT  
A method and device for laterally trimming an airplane during a flight is disclosed. The device (1) comprises means (6) for deflecting, in a dissymmetric way, flaps (4A, 4B) of the airplane so as...
US20150120090 METHODS AND SYSTEMS FOR DISPLAYING AIRCRAFT INFORMATION  
A method and an instrumentation system for an aircraft are provided. The method of presenting aircraft information includes activating a master indicator in response to a trigger event associated...
US20090248224 Integrated Air Navigation and Flight Control System  
A method and a device for solving air traffic congestions, improve safety, and reduce faults to simplify cockpit equipment. The method serves the navigation of airplanes from port to port with the...
US20140148979 NAVIGATION PERFORMANCE SPECIFICATION  
A method of formulating a specification for temporal and vertical required navigation performance is disclosed. The method assesses various flight management guidance systems methods and allows a...
US20050049762 Integrated flight management and textual air traffic control display system and method  
A system and method is provided for transmitting, receiving, initiating, and displaying textual air traffic control clearance messages simultaneously with a graphic representation of an aircraft...
US20150251772 SYSTEM AND METHOD OF MAPPING USER NOTES TO FLIGHT CHARTS  
A particular embodiment, a method includes receiving, at an electronic flight bag device, input corresponding to a user note. The method further includes generating, at the electronic flight bag...
US20130046422 ONBOARD FLIGHT PLANNING SYSTEM  
According to the application, a method for generating a flight route of an aircraft by an aircraft based computer system is disclosed. The method comprises the execution the following steps, which...
US20110024551 VARIABLE DAMPING OF HAPTIC FEEDBACK FOR A FLIGHT-ATTITUDE CHANGING LINKAGE OF AN AIRCRAFT  
The present invention relates to haptic feedback for operating at least one manual flight control device (21) for controlling the cyclic pitch of the blades (5) of a rotary wing (4) of a hybrid...
US20140018979 AUTONOMOUS AIRSPACE FLIGHT PLANNING AND VIRTUAL AIRSPACE CONTAINMENT SYSTEM  
Devices, systems, and techniques for generating a graphical user interface including a three-dimensional virtual containment space for flight of an unmanned aerial vehicle (UAV) are described. In...
US20090118875 Systems and methods for coordination of entities and/or communicating location information  
Systems and methods that may be employed to communicate location information between two or more aerial vehicles or other types of vehicles or other entities, and/or that may be used to facilitate...
US20120029736 Method for Dynamically Consolidating Items of an Aeronautical Procedure  
A method is provided for dynamically consolidating items of an aeronautical procedure in order to present to the operator the best action to perform according to the context of all the systems, in...
US20100310371 DRIVE CONTROL AND REGULATION METHOD AND SYSTEM FOR A HYBRID HELICOPTER  
The present invention relates to a control and regulation method for a rotorcraft having at least one variable-pitch propulsive propeller and at least one power source for driving the...
US20130046423 SYSTEM AND METHOD FOR AIRCRAFT THERMAL CAPACITY PREDICTION  
A technique for identifying, projecting, displaying, and enhancing the thermal capacity for an aircraft is disclosed wherein the thermal capacity is defined as the amount of time or range the...
US20140156115 METHOD FOR DISPLAYING AN AERONAUTICAL FLIGHT PLAN COMPRISING A STEP OF DISPLAYING AND SELECTING THE TASKS TO BE ACCOMPLISHED BEFORE A CHANGE OF FLIGHT PHASE  
The general field of the invention is that of methods of graphical representation, modification and validation of an aeronautical flight plan for an aircraft avionics system. Said system comprises...
US20110071709 HIGHLY REPRESENTATIVE REAL-TIME SIMULATION OF AN AVIONICS SYSTEM  
Optionally-mixed highly representative real time simulation of at least part of an avionics system (2). The simulation provides at least a step of translating communications interfaces into the...