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49results about How to "Data smoothing" patented technology

Method and system for testing dynamic stiffness

The invention relates to the field of traffic rails and specifically relates to a method and a system for testing dynamic stiffness. The method for testing the dynamic stiffness includes that a force in a preset frequency range is applied to a rail in preset time to enable the rail to produce vibration; force signals and vibratory acceleration signals are real-timely acquired according to a preset sampling frequency; data of the force F, time corresponding to the force F, data of an acceleration a and time corresponding to the acceleration a are recorded according to preset time intervals, the acquired force signals and the acquired acceleration signals; a corresponding relation of a displacement X and the frequency f is obtained according to the corresponding relation of the data of the acceleration a and the time corresponding to the acceleration a; the corresponding relation of the displacement X and the time t is obtained; and the corresponding relation of the dynamic stiffness Z and the frequency f is obtained according to the corresponding relations and the corresponding relation of the dynamic stiffness, the displacement and the force, and namely, wide frequency dynamic stiffness is obtained. By means of the method and the system for testing the dynamic stiffness, the wide frequency dynamic stiffness of the rail can be tested.
Owner:SOUTHWEST JIAOTONG UNIV

Attitude correction control system and method of a four-rotor aircraft

The invention discloses an attitude correction control system and method of a four-rotor aircraft. The control system comprises a flight control main controller, a flight attitude acquisition module,a driving module, a wireless communication module, a GPS module, a power management module and a camera module. The flight attitude acquisition module, the driving module, the wireless communication module, the GPS module, the power management module and the camera module are connected with the flight control main controller. An unmanned aerial vehicle attitude control system comprises a sensor data resolving and processing system, a motor rotating speed control system and a wireless data communication system. According to the invention, cascade PID closed-loop control is carried out on the attitude of the four-rotor aircraft, so that the PWM duty ratio for controlling the rotating speed of the motor is adjusted; and meanwhile, the four-rotor aircraft feeds back the position information obtained from the GPS module and current attitude data of the aircraft to a remote control terminal through a wireless transceiving module, so that the operator checks the current flight state of the aircraft in real time and thus descending processing is performed timely in an abnormal state of the flight to minimize the losses.
Owner:BEIJING UNIV OF TECH
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