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42results about How to "Improve flight experience" patented technology

Remote control terminal of unmanned flight vehicle, as well as flight auxiliary system and method of unmanned flight vehicle

The invention discloses a remote control terminal of an unmanned flight vehicle, as well as a flight auxiliary system and method of the unmanned flight vehicle, and belongs to the field of unmanned flight vehicles. The remote control terminal comprises an information acquisition module, an information processing module and an information output module; the information acquisition module is used for acquiring position information of an observation position, and acquiring position information and flight state information of the unmanned flight vehicle through a wireless network; the information processing module is used for acquiring the position information, relatively to the observation position, of the unmanned flight vehicle, according to the position information of the unmanned flight vehicle and the position information of the observation position; the information output module is used for outputting the flight state information of the unmanned flight vehicle and the position information of the unmanned flight vehicle relativley to the observation information. According to the remote control terminal of the unmanned flight vehicle, as well as the flight auxiliary system and method of the unmanned flight vehicle, a manipulator controls a flight path of the unmanned flight vehicle in an assisting manner through mastering the current flight position and the flight state of the unmanned flight vehicle; the blind flight and thw lost flight are prevented; meanwhile, the flight experience of the manipulators is improved.
Owner:SZ DJI TECH CO LTD

Unmanned plane driving simulation display unit

The invention provides an unmanned plane driving simulation display unit. According to the technical point, the unmanned plane driving simulation display unit comprises an unmanned plane, a remote controller and a cellphone. The unmanned plane is provided with a main control board and a lithium battery connected with the main control board. The main control board is provided with an ARM chip and a wifi module I connected with the ARM chip. The unmanned plane is provided with a camera. The camera is connected with the ARM chip. The remote controller is connected and communicated with the ARM chip through a wireless transceiving module. The ARM chip is connected and communicated with the cellphone through a wifi signal. The cellphone is put in a pair of virtual reality head glasses. Through adoption of the unmanned plane driving simulation display unit, the aerial photos of the unmanned plane can be transmitted to the cellphone in real time, and the photos on the cellphone screen can be seen through the virtual reality head glasses, so that the purpose of watching the aerial 3D photos of the unmanned plane is realized, the operator has the feeling of being personally on the scene, the authenticity of aerial simulation of the unmanned plane is improved, and the flight experience of the operator is improved.
Owner:宋克凡 +1

Design method of low-noise propeller of aircraft and propeller configuration

ActiveCN106114821AGood flying experienceImprove flight experiencePropellersLow noiseMomentum
The invention provides a design method of a low-noise propeller of an aircraft. The design method comprises the following steps of S100, according to a preset basic blade shape of the propeller of the aircraft, performing CFD calculation, namely computational fluid dynamics calculation, so as to obtain lift coefficients and resistance coefficients corresponding to different Reynolds numbers and different attack angles of the blade shape; S200, according to the preset flow state of environmental gas, the preset geometric parameters of the propeller, the lift coefficients and the resistance coefficients, performing momentum blade element theoretical calculation, so as to obtain aerodynamic data of the propeller; S300, according to the preset geometric parameters of the propeller and the aerodynamic data of the propeller, performing FW-H aeroacoutics equation calculation, so as to obtain noise characteristic data of the propeller; and S400, transferring an optimization algorithm based on a simulating annealing thought, and circularly executing the steps from S200 to S300 until the noise characteristic data is converged so that the best geometric parameters of the propeller is obtained. According to the design method disclosed by the invention, the power problem and the noise problem of the propeller are taken into account at the same time, and noises of the aircraft during a flight are greatly reduced.
Owner:SHENZHEN HIGHGREAT TECH DEV CO LTD

Flight mileage accumulation system based on frequent flyer card

The invention provides a flight mileage accumulation system based on a frequent flyer card. The flight mileage accumulation system is composed of a client system and a service end system. The client system comprises a client application module. The service end system mainly comprises a flight route extracting module and a mileage accumulation module. The flight route extracting module acquires an actual distance (S-kilometer) of a current flight route. The mileage accumulation module acquires reward rates V% of different cabins of a current airline company according to an airline company which is acquired by the flight route extracting module, and simultaneously acquires a reward rate T% of the frequency flyer card which belongs to the airline company. A mileage accumulation amount M which can be acquired by a flyer through taking the flight can be calculated in the mileage accumulation module through background data statistics and data sieving calculation according to a formula of M=(V%+T%)*S. The flight mileage accumulation system has advantages of supplying flight mileage accumulation data at this time in purchasing an air ticket by the flyer, satisfying a traveling requirement of the user, greatly improving user experience in flight, and furthermore perfecting a civil aviation searching system.
Owner:FEIYOU TECH CO LTD

Color correction method and system for multi-screen display of flight simulator

The invention provides a color correction method and system for multi-screen display of a flight simulator, and belongs to the technical field of flight simulators. On the basis of the color correction sample, predicting a CIE 1931 absolute tristimulus value when the display is driven at the same time to display, and taking the value as a color prediction value; a CIE 1931 absolute tristimulus value is used as a to-be-displayed target color representation form, a color correction model is established in combination with the color prediction value, and an optimal digital driving value required for displaying the target color is solved and determined; and the optimal digital driving value is utilized to control the display of a corresponding display, so that color correction of multi-screen display of the flight simulator is realized. According to the invention, accurate color control can be carried out on the visual system of the flight simulator, the problems of color distortion and inconsistent color development of multi-screen display of the flight simulator are solved, and the completely immersive flight experience of a driver in the flight simulator can be improved; and practical and effective technical support is provided for research, development, production and on-site correction of the flight simulator visual system.
Owner:BINZHOU UNIV

Unmanned aerial vehicle, control method and device thereof, remote control terminal and unmanned aerial vehicle system

An unmanned aerial vehicle, a control method and device thereof, a remote control terminal, and an unmanned aerial vehicle system are disclosed, the unmanned aerial vehicle system comprising an unmanned aerial vehicle (100) and a remote control terminal (200). The remote control terminal (200) is used for switching an auxiliary control part (220) of the remote control terminal from a non-trigger state to a trigger state when a first user instruction indicating that the auxiliary control part (220) is switched from the non-trigger state to the trigger state is obtained, and generating a first triggering signal; the first trigger signal is sent to the unmanned aerial vehicle (100); the unmanned aerial vehicle (100) is configured, when the unmanned aerial vehicle (100) is in a manual control mode, to enter an auxiliary control mode (S201) if a first trigger signal sent by the remote control terminal (200) is received; in the auxiliary control mode, if a first control signal transmitted by the remote control terminal (200) is received, a first target attitude of the unmanned aerial vehicle (100) is determined according to the first control signal (S202); an auxiliary attitude control quantity is determined according to the first target attitude and a first attitude of the unmanned aerial vehicle (100) corresponding to the preset state (S203); and the unmanned aerial vehicle (100) is controlled to rotate according to the first target attitude and the auxiliary attitude control quantity, so that the unmanned aerial vehicle (100) is in a preset state (S204).
Owner:SZ DJI TECH CO LTD
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