Matches 1 - 26 out of 26

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US20140110532 Direct-Drive Control of Aircraft Stability Augmentation  
According to one embodiment, a stability augmentation system includes a master linkage, a stability augmentation motor, and three linkages. A first linkage is coupled to the master linkage and...
US20130206898 Pilot Control System with Pendent Grip  
According to one embodiment, a control assembly includes a post, a grip, and a shaft. The post has a top, a bottom, and a body joining the top to the bottom. The shaft havs a first end coupled...
US20130256462 Unknown  
A piloting device (1) for piloting a vehicle, in particular an aircraft, has a frame (10), a cradle (20) pivoting with respect to the frame on a first pivot axis (R), a piloting member, called a...
US20080258014 AIRCRAFT KINETIC LANDING ENERGY CONVERSION SYSTEM  
A kinetic energy system which transfers the kinetic landing into recoverable electric energy for an aircraft. The system incorporates at least one wheel supporting the aircraft for landing and...
US20140001313 MECHANICAL CONTROL MIXER AND METHOD THEREFOR  
A mechanical control mixer configured to couple to an aircraft is provided. An axle is mounted to a frame of the mechanical control mixer, and a barrel is configured to rotate about the axle. A...
US20120032032 Air-Vehicle Integrated Kinesthetic Control System  
A lift platform with a kinesthetic control system that is coupled to means for altering air flow through the first and second longitudinally-spaced ducts comprising the lift platform is provided....
US20070235593 Flying control device for a rotorcraft  
The invention relates to a rotorcraft cockpit having a left seat and a right seat placed side-by-side, a console extending between the seats, two side sticks, one situated to the right of the...
US20150076288 METHOD AND DEVICE FOR AIDING THE CONTROL OF AN AIRCRAFT DURING A PARABOLIC FLIGHT IN ORDER TO GENERATE WEIGHTLESSNESS IN THE AIRCRAFT  
Method and device for aiding the control of an aircraft during a parabolic flight in order to generate weightlessness in the aircraft. The device includes an unit for automatically calculating a...
US20080272243 Control apparatus for an aircraft  
The present invention relates to a control apparatus for an aircraft comprising a multiaxially tiltable joystick for the actuation of at least two control transducers for the pitch and roll...
US20140091181 CONTROLLER  
A controller includes a first body portion, adapted to be grasped by a person's middle finger, ring finger, and pinky finger, a second body portion adapted to be grasped by a person's index...
US20100023239 POWER DEMAND MANAGEMENT  
A method is disclosed of determining the power demand on a power subsystem (2) of a system (1) by optimising a respective demand-dependent operating characteristic based on one or more operating...
US20090242691 SWASHPLATE TRAJECTORY CONTROL  
A system and method of controlling a rotary-wing aircraft includes transforming a non-rate limited servo position command into a rate limited servo position command.
US20080197239 Method and Device for Driving an Aircraft During the Ground Run Thereof  
The inventive method consists in forming a difference (D1) between left and right braking commands (FG, FD), in converting said difference (D1) into an additional control command (D2) for rudder...
US20090146018 Control device  
The invention relates to a control device, in particular for an aircraft, having a multiaxially tiltable joystick for the actuation of signal transducers, in particular for the pitch control and...
US20100064823 Sensor System for Monitoring the Synchronism of Control Surfaces of an Aircraft  
The present invention relates to a sensor system for monitoring the synchronism of control surfaces of an aircraft with two transmission links for the mechanical transmission of the movements of...
US20080001037 Actuator link assembly, flight control system and method of making same  
An actuator link assembly includes a sleeve member with a sleeve lug on one end. The sleeve lug is a split lug having primary and secondary lug portions. There is a coupling fixture on the sleeve...
US20100305780 FLIGHT CONTROL SYSTEM AND METHOD OF SEPARATING CONTROL LEVER LINKAGE  
A flight control system according to the present invention includes a first sensor, a flight control computer, a link mechanism, a separation unit, and a second sensor detecting a force...
US20150158595 AIRCRAFT THROTTLE CONTROL SYSTEM WITH AN EMITTER UNIT AND A RECEIVER UNIT  
An aircraft throttle control system having a control lever. The control system comprises an emitter unit having the pivot-mounted control lever and a receiver unit having a pivot-mounted lever,...
US20090302170 ROTATIONAL AIRCRAFT THROTTLE INTERFACE  
An aircraft control input apparatus is configured to accept and provide to the aircraft control inputs from a user regarding the magnitude and direction of the aircraft's thrust vector. The...
US20140346280 System And Method For Controlling An Aircraft  
A system for controlling an aircraft control parameter including a control interface including a mobile element configured to move on a travel, of which at least two portions are separated by a...
US20110006166 ROTARY WING VEHICLE  
A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to...
US20120032031 CONTROL SYSTEM  
The invention relates to a control system and to a method of operating such a control system, particularly to a control system for pilot command inputs for a helicopter, with a mechanical input...
US20170015410 METHODS AND CONTROL SYSTEMS FOR CONTROLLING A DRIVE SYSTEM OF AN AIRCRAFT  
A method of controlling a drive system of an aircraft. The drive system comprised a drive motor arranged to drive at least one wheel of an aircraft landing gear. A power signal indicative of a...
US20160280392 WINGTIP CONTROL SYSTEM  
A method and apparatus for a wingtip control system. The wingtip control system comprises a switch system for a flight deck of an aircraft and a controller. The switch system is configured to be...
US20150266591 METHOD AND A DEVICE FOR ISSUING TERRAIN AVOIDANCE WARNINGS FOR A ROTARY WING AIRCRAFT  
A method and a device (50) for issuing a terrain avoidance warning for a rotary wing aircraft (100) during which at least one bundle (N1, N2) of possible avoidance trajectories for said aircraft...
US20100327122 Air-vehicle augmented kinesthetic control system  
An augmented kinesthetic control system for use with a lift platform, the lift platform comprising first and second longitudinally-spaced thrust generating means, is provided. The first and second...
Matches 1 - 26 out of 26