Match Document Document Title
6385513 Satellite emergency voice/data downlink  
A satellite emergency voice/data downlink method and apparatus that sends cockpit audio and flight data to a satellite communications system upon detection of a serious event or a pilot generated...
6381517 Method and apparatus to analyze accessor performance  
An automated data storage system which comprises one or more robotic accessors movably disposed therein, each such accessor including a revolving memory buffer and a velocity control program,...
6381519 Cursor management on a multiple display electronic flight instrumentation system  
An aircraft display and control system generally includes a processor, a cursor control and selection device, an aeronautical information database, a geographic database, and a plurality of display...
6380869 Automated air-traffic advisory system and method  
A method and apparatus for automatically providing advisories to pilots in a monitored airspace comprises monitoring weather conditions and air traffic in an airspace and then generating and...
6370457 Debriefing systems and methods for retrieving and presenting multiple datastreams with time indication marks in time synchronism  
Event debriefing systems and methods are provided for recording a plurality of datastreams related to an event. An observer of the event may create time indication marks that facilitate recalling,...
6370450 Integrated total temperature probe system  
A smart probe system for an aircraft receives an input from a heated total air temperature sensor. When on the ground, the heater for the total air temperature probe is cycled so that when a...
6367031 Critical control adaption of integrated modular architecture  
The present invention, Layered Detection Architecture (“LDA”) is useful to enhance the detection of command control processing errors and also facilitate survivorship among properly functioning...
6366835 Height estimating apparatus  
Apparatus for estimating a first height ( 1 ) of a vehicle ( 2 ) above a first reference surface ( 3 ), including a system ( 4 ) for determining position, velocity and attitude incorporating at...
6363325 Automotive emergency awareness system  
A vehicular emergency awareness system and method is provided. A vehicle is provided with an onboard computer system adapted to receive and process signals generated at an external source. Under...
6353790 Gas turbine aeroengine control system  
In a control system for a gas turbine aero engine, the control system (ECU) is configured as a dual control system comprising two channels, Ch-A and Ch-B. Ch-A has two CPUs which conduct...
6353779 Method for managing communication modes for an aircraft  
The present invention relates to the management, on board an aircraft, of the aeronautical digital telecommunications networks ACARS and ATN. It covers a method for automatic choice of the...
6346892 Method and apparatus for aircraft systems management  
Aircraft and other systems employing various condition settable parameters are controlled utilizing a command language, display, and input device for entering certain desired parameters with a...
6347263 Aircraft terrain information system  
An aircraft terrain warning generator is provided having a terrain and obstacle warning envelope having a lower boundary formed according to the lesser of the current aircraft flight path angle and...
6345232 Determining aircraft position and attitude using GPS position data  
The present invention is a method and apparatus to determine flight parameters of an aircraft. Data received from a global positioning system (GPS) receiver are converted to position data. The...
6336062 Attitude angle sensor correcting apparatus for an artificial satellite  
An attitude angle sensor correcting apparatus for an artificial satellite of the present invention includes a satellite attitude estimator. The satellite attitude estimator reads geographical image...
6320579 Cockpit display having 3D flight path error symbology  
A primary flight display (PFD) for an aircraft generating a 3-dimensional (3D) symbology indicative of the aircraft situational information. The 3D symbology includes a 3D vertical path error...
6317659 Layered subsystem architecture for a flight management system  
An improved aircraft flight management system (FMS) based on a layered subsystem architecture, residing on a computing platform and including an operator interface subsystem, a communications...
6314343 Aircraft flight mode selector system  
An aircraft flight mode selector assembly utilizes computer-generated menus and soft wired bezel keys to enable the use of a greater number of flight modes to be accessed in a smaller space than is...
6314350 Methods and apparatus for generating maintenance messages  
Sensor selection status monitoring and maintenance logic for generating messages relating to intermittent and "in-range" faults are described. In one embodiment, a transition count is generated...
6313759 System and method of communication between an aircraft and a ground control station  
A system for communicating between an aircraft and a ground control station. The system includes a communications module disposed onboard the aircraft and capable of electronically communicating...
6311107 Wind advisory system  
The present invention is a two-part wind advisory system comprising a ground station at an airfield and an airborne unit placed inside an aircraft. The ground station monitors wind conditions (wind...
6308044 System and method of providing OOOI times of an aircraft  
A method for determining the "Out," "Off,". "On," and "In" (OOOI) times for an aircraft, based on parametric data sampled in the aircraft. "Out" means out of the gate, "Off" means off the ground,...
6304194 Aircraft icing detection system  
The present invention comprises a system and method for detecting icing conditions in a multi-mode aircraft by indirectly detecting ice accretion through the measurement of aircraft performance...
6292720 Trimming process for adapting a simulation system to an automatically controlled reference system  
Trimming process for adapting a first control loop of a controllable, automatically controlled reference system, which is or represents an aircraft, to a second control loop which simulates the...
6289289 Aircraft structural fatigue monitor  
The present invention is a system for monitoring, storing, and reporting the accumulation of fatigue occurrences experienced by an aircraft. The system according to the present invention uses...
6282466 Method of automated thrust-based roll guidance limiting  
An improvement to a method of automatic flight using a flight management system is provided. The flight management system includes a lateral navigation (LNAV) control mode in which the flight...
6281810 Redundant avionics for critical flight instruments  
Redundant avionics for flight instruments: a plurality of aircraft flight data sensors, which provide data that are normally displayed on indicators in the cockpit, are transmitted to two...
6278913 Automated flight data management system  
A data processing system for automating the process of managing flight data and generating reports based on that data. The system accesses flight data transmitted on an airborne databus, where the...
6275769 Weight and balance calculator for aircraft  
A hand-held computer that displays the aircraft floor plan with passenger and baggage compartments shown on a pad, with which a pilot can calculate the Center of Gravity (CG) of an aircraft by...
6273371 Method for interfacing a pilot with the aerodynamic state of the surfaces of an aircraft and body interface to carry out this method  
Method, apparatus and sensors for directly interfacing a pilot (1) with the aerodynamic state of the surfaces of an aircraft, in particular allowing the direct sensorization of the conditions of...
6266583 System and method for improving the accuracy of pressure altitude determinations in an inertial navigation system  
A system and method for improving the accuracy of altitude determinations in an inertial navigation system. Pressure measurements available to the inertial navigation system are used to initially...
6259975 Flight control system for an aircraft particularly for a helicopter  
A flight control system for an aircraft, particularly for a helicopter receives a number of items of information, especially the position of flight control members of said aircraft, and sends,...
6259977 Aircraft flight data analysis system and method  
An aircraft data analysis computer program and method that allows user-defined measurements to be made on a set of flight data obtained from a variety of sources. Post-flight measurement and...
6259380 Method and apparatus of automatically monitoring aircraft altitude  
An apparatus and method for automatically and independently determining aircraft altitude and alerting the pilot to deviations from a target altitude exceeding a specified tolerance. The alerter...
6253126 Method and apparatus for flight parameter monitoring and control  
Methods and apparatus are disclosed for three-dimensional flight control based generally upon measuring and comparing actual air pressures at or near various surfaces of an aircraft during flight....
6253166 Stable algorithm for estimating airdata from flush surface pressure measurements  
An airdata estimation and evaluation system and method, including a stable algorithm for estimating airdata from nonintrusive surface pressure measurements. The airdata estimation and evaluation...
6246341 Method and device for assistance with the maintenance of an aircraft, especially of a helicopter  
The present invention relates to a method and a device (1) for assistance with the maintenance of an aircraft, especially of a helicopter, intended for replaying maintenance information. According...
6240341 Flight management system (FMS) with integrated bit mapped data charts  
An aircraft Flight Management System (FMS) simultaneously displaying FMS navigation data and geographically referenced bitmap data charts. The bitmap data charts are properly registered with the...
6236913 Method and device for inputting and controlling flight data  
6236912 Process and device for aiding aerial navigation, with display of navigation instruments used  
A process and device for assisting aerial navigation. The system affords the pilot of the aircraft greater knowledge regarding the situation which results from automatic decisions of a flight...
6236914 Stall and recovery control system  
An autopilot controller, for controlling a vehicle traveling in a fluid medium, designed for controlling the vehicle in any one of pre stall, stall and post stall regions. The autopilot controller...
6219618 Aircraft navigational warning system  
An aircraft navigational system allows for reduced storage and increased computing power for comparing terrain maps to the flight path and enroute track of the aircraft. Unique provisions are made...
6216063 On-line μ method for robust flutter prediction in expanding a safe flight envelope for an aircraft model under flight test  
A structured singular value (μ) analysis method of computing flutter margins has robust stability of a linear aeroelastic model with uncertainty operators (Δ). Flight data is used to update the...
6199008 Aviation, terrain and weather display system  
A computer system for displaying terrain, weather and aviation information includes a terrain database, an aviation map database, a weather database, an air traffic database, an airplane specific...
6188937 Methods and apparatus for annunciation of vehicle operational modes  
A vehicle control system contains a behavior annunciation function for generating a behavior mode output. The behavior mode annunciation system has a vehicle operational parameters database and a...
6181990 Aircraft flight data acquisition and transmission system  
An aircraft data transmission system used with an aircraft having a data acquisition unit. The system includes a communications unit located in the aircraft and in communication with the data...
6181987 Method of assistance in the piloting of an aerodyne  
The disclosed method is implemented by a system aboard an aerodyne comprising a processor, a terminal and memories in which there are stored all the information necessary for the carrying out of a...
6175314 Voice annunciation of data link ATC messages  
A system for voice announcing air traffic controller to pilot data link communication messages of a type which are in conformance with predetermined industry standard message formats, the system...
6173159 Wireless spread spectrum ground link-based aircraft data communication system for updating flight management files  
A system and method updates flight management files in accordance with the present invention and provides a retrievable record of the flight performance of an aircraft. A flight management computer...
6173220 Attitude direction indicator with supplemental indicia  
An attitude direction indicator (ADI) display includes a horizon line that divides an upper colored portion, which represents the sky, from a lower colored portion, which represents the Earth. The...