#B64C19/00

POWER GENERATION CONTROLLER OF AN AIRCRAFT

A power generation controller of an aircraft includes a low-temperature start-up control section and a power generation control section. When it is determined that an oil temperature of a hydraulic ac…

DRIVE·Jan 3·1 min read

B64C19/00 KAWASAKI HEAVY IND LTD [JP]

METHODS AND APPARATUS FOR GLOBAL OPTIMIZATION OF VERTICAL TRAJECTORY FOR AN AIR ROUTE

A method for calculating vertical trajectory values is provided. The method obtains aircraft performance data for a particular aircraft and atmospheric condition data associated with an air route; cal…

DRIVE·Nov 9·1 min read

B64C19/00 HONEYWELL INT INC [US]

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 associated…

DRIVE·Dec 31·1 min read

B64C19/00 HONEYWELL INT INC [US]

System to assist with maintaining the hovering of a helicopter

The system has a pilot symbol generating unit (GS) provided in helmet display at virtual positions fixed relative to a terrestrial mark (RT) to compute representations comprising targets when a helico…

DRIVE·Mar 5·1 min read

B64C19/00 THALES SA [FR]

Method and device for assisting the flight management of an aircraft

The method involves allowing a pilot to enter setpoints such as speed setpoint and altitude setpoint, by a flight control interface unit (2). An interface unit (4) is envisaged for allowing the pilot …

DRIVE·Feb 5·1 min read

B64C19/00 AIRBUS OPERATIONS SAS [FR]

Method for providing a description of aircraft intent using a decomposition of flight intent into flight segments with optimal parameters

The present invention provides a computer-implemented method of generating a description of aircraft intent expressed in a formal language that provides an unambiguous description of an aircraft's int…

DRIVE·Nov 27·1 min read

B64C19/00 BOEING CO [US]

Backup instrument for an aircraft

The instrument (10) has an inertial sensor (1) and a pressure sensor (2) connected to a calculation unit (3) that determines critical flight information for an aircraft. The calculation unit includes …

DRIVE·Oct 23·1 min read

B64C19/00 EUROCOPTER FRANCE [FR]

Method and apparatus for generating heading error data used by an Electronic Flight Director

An improved Horizontal Situation Indicator module for use with an aircraft, wherein the HSI module is adapted for accepting Bank Angle Commands or waypoint data from a GPS flight module and for using …

DRIVE·Oct 16·1 min read

B64C19/00 L 3 COMM CORP [US]

Geodesic marking system for marking target points

The system (1) has geodetic position determination arrangement (20) to determine external actual position of automotive, unmanned, remotely controllable air vehicle (10) such as aircraft. A control un…

DRIVE·Oct 17·1 min read

B64C19/00 HEXAGON TECHNOLOGY CT GMBH [CH]

Method and device for controlling the operating speed of the engines of an aircraft during the take-off phase

The method involves measuring current values (N1c1-N1c4) of driving parameters associated to external engines (M1, M4) and internal engines (M2, M3). Detection is made whether difference between the c…

DRIVE·Oct 10·1 min read

B64C19/00 AIRBUS OPERATIONS SAS [FR]

Aircraft takeoff

The present invention provides a method of operating an aircraft whereby actual acceleration of an aircraft is used as the direct measure of the capability of the aircraft to takeoff. Thus, a minimum …

DRIVE·Jan 18·1 min read

B64C19/00 ROLLS ROYCE PLC [GB]