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US20100295303 Tethered system for power generation  
A system for power generation comprises a wing, a turbine, a tether, and a tether tension sensor. The wing is for generating lift. The turbine is coupled to the wing and is used for generating...
US20140365041 METHOD FOR MANAGING A VERTICAL FLIGHT PLAN  
A method for managing a vertical flight plan comprises: a first step of breaking down an initial flight plan into a succession of contiguous segments, each segment comprising a change of altitude...
US20150142223 EVALUATING AILERON DEFLECTION WHILE AN UNMANNED AERIAL VEHICLE IS IN FLIGHT  
A technique is directed to operating a UAV. The technique involves launching (or guiding) the UAV into flight. The technique further involves performing a series of aileron (or other control...
US20130060406 Flight Control Laws for Vertical Flight Path  
A flight control system and method for controlling the vertical flight path of an aircraft, the flight control system includes a stable decoupled model having a decoupled lateral equation of...
US20130090788 FLIGHT CONTROL LAWS FOR FULL ENVELOPE BANKED TURNS  
A flight control system and method for controlling full envelope banked turns of an aircraft, the flight control system including one or more of a control law architectures having one or more...
US20150251756 SYSTEM AND METHOD FOR COMMANDING A PAYLOAD OF AN AIRCRAFT  
A system and method is provided for commanding a payload of an aircraft. A plurality of flight segments, which comprise trajectory information of the aircraft, are received. A plurality of payload...
US20140172202 SYSTEMS AND METHODS FOR SAFELY LANDING AN AIRCRAFT  
A system for safely landing an aircraft including a low range radio altimeter, a barometric altimeter, and an autothrottle control. The low range radio altimeter calculates a first height of the...
US20120226395 METHOD AND SYSTEM FOR DETERMINING THE ATTITUDE OF AN AIRCRAFT BY MULTI-AXIS ACCELEROMETRIC MEASUREMENTS  
An inertial system measures the attitude of an aircraft consisting at least in determining the angle of pitch and/or the angle of heading and/or the angle of roll of the aircraft, each of the said...
US20140336849 SYSTEM AND METHOD FOR DISPLAYING RATE-OF-CLIMB ON AN AVIONICS VERTICAL SPEED INDICATOR  
A system and method are providing for providing an aircraft with adequate clearance over an obstacle in the aircraft's takeoff departure path. The correct rate-of-climb to clear the obstacle is...
US20110172854 System and method for effecting vehicle maneuver to compensate for IMU error  
The effects of IMU gyro and accelerometer bias errors are significantly reduced in accordance with the present teachings by a system or method for commanding an IMU or vehicle through a series of...
US20140236399 Method and device for estimating an unwanted pitch moment of an aircraft, and applications to the pitch control of the aircraft  
A method and device for estimating an unwanted pitch moment of an aircraft, and applications to the pitch control of the aircraft. The device estimates an unwanted pitch moment, which can be used...
US20140244077 METHOD FOR CREATING A VERTICAL TRAJECTORY PROFILE COMPRISING MULTIPLE ALTITUDE LEVELS  
A method for creating a vertical trajectory profile of an aircraft by optimization of a criterion representative of a flight cost, comprises: performing a first iterative computation of a profile...
US20140343760 METHOD AND DEVICE FOR AUTOMATICALLY DETERMINING AN OPTIMIZED APPROACH AND/OR DESCENT PROFILE  
A method and device for automatically determining an optimised approach and/or descent profile for an aircraft are provided. The device comprises means for optimising an approach and/or descent...
US20110054719 METHOD FOR DRAMATICALLY REDUCING THE TAKE-OFF RUN OF AN AIRCRAFT  
According to the invention, during take-off, the aircraft (AC) is given an attitude (θc) close to the tail-touching attitude and the ailerons (6G, 6D) are fully deflected downwards.
US20120022723 Method And Device For Determining And Updating A Target Altitude For An Emergency Descent Of An Aircraft  
Method and device for determining and updating a target altitude for an emergency descent of an aircraft The device (1) includes means (3, 4, 8, 10) for determining a target altitude from a...
US20150032298 AIRCRAFT FLIGHT DECK DISPLAYS AND SYSTEMS AND METHODS FOR DISPLAYING INTEGRATED MINIMUM SAFE ALTITUDE AND MINIMUM VECTORING ALTITUDE INFORMATION ON A DISPLAY DEVICE IN AN AIRCRAFT  
A method is provided for displaying integrated minimum vectoring and safe altitude information on a display device in an aircraft. The method comprises displaying a graphical representation of a...
US20110130895 METHOD OF OBTAINING A LOCAL TERRAIN ELEVATION DATABASE FROM DETECTOR MEANS ON BOARD A VEHICLE  
A method essentially comprising a step of storing each plot mesh. Each plot mesh receiving plots sent thereto by detector means and retaining in memory at least the altitude of the highest plot...
US20120253562 Method And Device For Automatically Managing The Vertical Profile Of The Flight Plan Of An Aircraft  
The device includes means for determining a plurality of successive standard flight sections (S1A, S2A, S3A, S4A) comprising a level and a transition phase for reaching this level, and means for...
US20060293804 Aircraft vertical speed instrument device with multi-functional design aspects  
The present invention provides a unique and novel device for indicating flight information to a pilot or co-pilot of an aircraft. The present invention is adapted to fit into an existing aircraft...
US20060004496 Enhanced vertical situation display  
A vertical situation display system for use in a vehicle such as, for example, an aircraft, is provided. A side view of an intended route of flight may be shown with altitude restrictions,...
US20140350748 INVERTED-LANDING AIRCRAFT  
An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an...
US20110295449 METHODS AND SYSTEMS FOR REDUCING ANGULAR VELOCITY USING A GYROSCOPE ARRAY  
Methods and systems are provided for reducing angular velocity of a vehicle using a gyroscope array. A method comprises dithering a gyroscope of the gyroscope array, obtaining current through a...
US20130173091 EARLY IDENTIFICATION OF A VORTEX RING PHASE  
The invention relates to a method for early detection of the vortex ring state in a helicopter, having the following steps: establishing flight control signals for flight control with regard to...
US20110224848 APPARATUSES AND METHODS FOR DISPLAYING AND RECEIVING TACTICAL AND STRATEGIC FLIGHT GUIDANCE INFORMATION  
Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying...
US20070043482 Emergency descent system  
An emergency descent system is provided for automatically performing an emergency descent in a vehicle. The system monitors cabin pressure altitude and if the cabin pressure altitude exceeds a...
US20090088911 METHOD AND SYSTEM FOR MANEUVERING AN AIRCRAFT BY SHIFTING ITS CENTER OF GRAVITY  
A method to maneuver an aircraft in flight, in which the center of gravity of the aircraft is shifted by transferring fuel from at least one first fuel tank to at least one second fuel tank of the...
US20090326741 DEVICE AND METHOD FOR EXTRACTING TERRAIN ALTITUDES  
The present invention relates to a method and a device for extracting terrain altitudes notably for a display of a sectional view of a terrain overflown by an aircraft. The device for extracting...
US20120158219 TRAJECTORY BASED SENSE AND AVOID  
A trajectory-based sense-and-avoid system for use on an aircraft is provided that utilizes 4-D constructs, such as 4-D trajectories or 4-D polytopes, to maintain separation from other aircraft...
US20140058593 LOW-ALTITUDE ALTIMETER AND METHOD  
A low-altitude altimeter (10) and a method of determining low altitudes for unmanned aerial vehicles (24). The altimeter includes at least two illuminators (12, 14), at least one sensor (16), and...
US20130151040 LOW-ALTITUDE ALTIMETER AND METHOD  
A low-altitude altimeter (10) and a method of determining low altitudes for unmanned aerial vehicles (24). The altimeter includes at least two illuminators (12,14), at least one sensor (16), and a...
US20130190951 PRESSURE ALTITUDE STABILIZATION  
A method and apparatus is provided for determining the altitude of an aircraft. In accordance with the method, Global Positioning Satellite (GPS) data is received from a plurality of GPS...
US20080195263 Altimeter setting display and storage system and method  
A system and method for storing altimeter setting values on an aircraft display includes simultaneously rendering an altimeter and an active altimeter setting field, and selectively rendering a...
US20110202208 METHOD AND SYSTEM FOR PREDICTING PERFORMANCE OF AN AIRCRAFT  
Methods and systems for operating an avionics system on-board an aircraft are provided. A plurality of signals representative of a current state of the aircraft are received. A future state of the...
US20100305783 ENHANCED VERTICAL SITUATION DISPLAY  
A vertical situation display system for use in a vehicle such as, for example, an aircraft, is provided. A side view of an intended route of flight may be shown with altitude restrictions,...
US20080125920 Unmanned Airborne Vehicle For Geophysical Surveying  
An un-manned airborne vehicle (UAV), for acquiring aeromagnetic data for geophysical surveying at low altitude on land or over water, comprising an extended fuselage that is adapted to hold and...
US20060271249 Adjustment of altitude measurements  
This disclosure describes novel systems, methods and software for determining a position of a tracked object, which might be a fixed-wing or rotary-wing aircraft, some other flying object, a...
US20100042271 METHOD AND DEVICE FOR MOVEABLE TAIL TRIMMING IN AN AIRCRAFT  
The invention relates to a method for actuating an adjusting drive for adjusting an elevator (12) and an adjusting drive for adjusting a moveable tail (23) provided with the steps: Generation of...
US20090171517 Shooshoo  
According to a preferred embodiment of present invention, a method and apparatus for Computer Controlled tail-rotor anti-torque system, utilizing stored momentum of rotating body as well as power...
US20080077284 System for position and velocity sense of an aircraft  
A system for determining the position and/or velocity of an autonomous aircraft in a low-cost, low-weight manner independent of external technological dependencies such as satellites or beacons is...
US20130179010 SYSTEM AND METHOD FOR INDICATING A PERSPECTIVE COCKPIT FIELD-OF-VIEW ON A VERTICAL SITUATION DISPLAY  
An aircraft display system is provided and configured to render a cockpit display having a field-of-view. The system comprises a monitor and a processor coupled to the monitor and configured to...
US20090230253 METHOD AND DEVICE FOR PILOTING AN AIRCRAFT OPTIMIZING THE CONTROL OF THE AILERONS IN AN ENHANCED-LIFT CONFIGURATION  
In conformance with the invention, based on the incident conditions and velocity, the steering of the ailerons is weakly negative (b0) or corresponds either to the maximum sharpness of the...
US20080119970 Precision Approach Guidance System And Associated Method  
A precision approach guidance system that provides flying craft guidance information during a precision approach to a landing site and methods associated therewith are provided. In one embodiment,...
US20150203214 METHOD AND DEVICE FOR VERTICALLY GUIDING AN AIRCRAFT DURING AN APPROACH OF A RUNWAY ALONG A LATERAL APPROACH TRAJECTORY  
A method and device including a unit to extract a linear terrain profile stored in memory, a terrain height for a current distance of the aircraft, a unit for determining a current height of the...
US20050143872 Aircraft gps instrumentation system and relative method  
The present invention refers to an instrumentation system of an aircraft by means of GPS (Global Positioning System). In particular, it refers to a modular instrumentation system for aircraft,...
US20130024052 SYSTEMS AND METHODS FOR GENERATING A COMMAND TRAJECTORY  
A system for use in generating a command trajectory for an aircraft is provided. The system includes a natural frequency determining module configured to determine a closure rate of the aircraft...
US20090024259 Stores dependent angle of attack feedback  
A method for adjusting angle of attack feedback gain based characteristics and position of mounted stores, and a control system using the method.
US20120095623 DEVICE FOR ASSISTING AIRCRAFT CREW WHEN PERFORMING FLIGHT LEVEL CHANGES  
This device providing assistance to aircraft crew for a flight level change of the aircraft in air traffic, comprising means for viewing the position of the aircraft in the vertical plane, is...
US20100025524 FORCE GRADIENT USING A NON-CONTACT PROXIMITY SENSOR  
An improved design for a force gradient using a proximity sensor is disclosed. A force gradient comprises a shaft having a first end and a second end. The switch includes a spring contained...
US20110046823 PROCESS AND DEVICE FOR OPTIMISING THE PERFORMANCE OF AN AIRCRAFT IN THE PRESENCE OF A LATERAL DISSYMETRY  
A process and device for optimising the performance of an aircraft in the presence of a lateral dissymmetry is disclosed. The device (1) includes means (2, 3, 4, 5, 7, 9) for controlling, during a...
US20090187292 INTEGRATED PITCH, ROLL, AND YAW INCEPTOR  
A method and apparatus for a control system for an aircraft. The control system comprises a grip, a set of feedback components connected to the grip, and a set of sensors. The set of feedback...
Matches 1 - 50 out of 235 1 2 3 4 5 >