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1186 results about "Yaw" patented technology

A yaw rotation is a movement around the yaw axis of a rigid body that changes the direction it is pointing, to the left or right of its direction of motion. The yaw rate or yaw velocity of a car, aircraft, projectile or other rigid body is the angular velocity of this rotation, or rate of change of the heading angle when the aircraft is horizontal. It is commonly measured in degrees per second or radians per second.

Dynamic detection method for preventing wagon from turning towards one side on bending road and pre-warning apparatus

The invention relates to a rollover prevention dynamic detection method for a wagon on a curved conduit and a warning device. The method comprises the following steps: 1, installing a rollover prevention dynamic detection method for a wagon on a curved conduit which comprises a steering wheel rotation angle measuring device, a yaw angle velocity measuring device, an inclination angle measuring device and an electronic control unit which comprises a single chip microcomputer, wherein a solidification program of the single chip microcomputer is equipped with a centroid height dynamic detection algorithm module and a rollover prevention warning algorithm module, and a rollover alarming range is arranged in the rollover prevention warning algorithm module. 2, collecting steering wheel rotation angle singles, vertical yaw angle velocity measuring singles of the wagon, side-tipping angle singles of a carriage of the wagon, the side-tipping angle singles of a rear shaft of the wagon and vertical speed singles of the wagon. 3, a lateral acceleration and a centroid height of the wagon is counted through the centroid height dynamic detection algorithm module. 4, counting a rollover acceleration threshold value through the rollover prevention warning algorithm module according to the centroid height. 5, sending a corresponding alarm command according to a difference value of the lateral acceleration and the rollover acceleration threshold value of the wagon and the reset rollover alarm range.
Owner:TSINGHUA UNIV

Lane departure alarming method and system with driving distraction state considered

InactiveCN103661375AAdjust system parameters in real timeIncrease driving distraction detection functionExternal condition input parametersSignalling/lighting devicesInformation controlSteering wheel
Provided is a lane departure alarming method with a driving distraction state considered. The method comprises the steps that whether a driver is in a distracted driving state at present is judged according to the traveling track of an automobile and the operation information of the driver; distinguished alarming strategies are provided according to the detecting result of distracted driving, and when driving distraction is not detected, the time for lane departure alarming is delayed. A lane departure alarming system for achieving the method comprises an environment sensing unit, an information control unit, a data processing unit, a distraction detecting unit, a road virtual unit and an alarm decision making unit. The yaw angle of the automobile and the rotating speed signal of a steering wheel are acquired from the environment sensing unit and the information control unit, corresponding standard deviation statistical data can be obtained after data processing, and driving distraction detection is conducted. The alarm decision making unit makes alarm decisions, and judges whether the current alarm signal is restrained or not. The lane departure alarming method and system can provide the distraction driver with timely lane departure alarm, and meanwhile avoid frequent false alarm to the focused driver so that disturbing to the driver can be reduced.
Owner:TONGJI UNIV

Hypersonic speed aircraft control method capable of suppressing constant deviation influence of sideslip angle signal

The invention discloses a hypersonic speed aircraft control method capable of suppressing the constant deviation influence of a sideslip angle signal. The method comprises the following steps: (1) measuring the yaw angle speed omega y and the roll angle speed omega x of an aircraft in real time by utilizing an inertial measurement unit, and acquiring a roll angle gamma and a sideslip angle by utilizing the inertial measurement unit and a sensor; (2) calculating a deviation signal of the gamma and a roll angle instruction gamma c, integrating a deviation signal Delta gamma, and performing the amplitude limiting on the deviation signal, so as to obtain a roll angle integrated signal; (3) amplifying the roll angle integrated signal and the omega y, generating a control instruction, and feeding the control instruction back to a rudder of the aircraft; amplifying the omega x, generating a control instruction I and feeding the control instruction I back to an aileron of the aircraft; amplifying the Delta gamma, generating a control instruction II and feeding the control instruction II back to the rudder / aileron of the aircraft; (4) adding all the control instructions which are fed back to the rudder to serve as a general control instruction of the rudder, and controlling the rudder to track the general control instruction through a servo system on the aircraft; adding all the control instructions I fed back to the aileron to serve as a general control instruction I of the aileron, and controlling the aileron to track the general control instruction through the servo system on the aircraft.
Owner:CHINA ACAD OF LAUNCH VEHICLE TECH

Path planning obstacle avoidance control method for autonomous underwater vehicle in large-scale continuous obstacle environment

ActiveCN112241176AFast convergenceReal-time obstacle avoidance capabilityAltitude or depth controlComputer control systemModular design
The invention relates to a path planning obstacle avoidance control method for an autonomous underwater vehicle in a large-scale continuous obstacle environment. The invention relates to the technicalfield of underwater robot path obstacle avoidance planning, and the method comprises the steps: building a large-scale continuous obstacle simulation training environment, building the state and action of a deep reinforcement learning neural network through employing obstacle avoidance sensor information as the input and the navigation speed and yaw angular speed as the output, for a multi-targetstructure of a motion planning obstacle avoidance control process, performing modular design on a reward function, and in order to avoid system instability caused by sparse rewards, setting continuous rewards are set in combination with an artificial potential field method. According to the method, obstacle avoidance training is carried out on the autonomous underwater vehicle by utilizing an improved depth deterministic strategy gradient algorithm, and an obstacle avoidance strategy obtained by training is written into a robot lower computer control system; when the autonomous underwater vehicle runs in an underwater canyon, obstacle avoidance is carried out by using an obstacle avoidance strategy learned by training, and the autonomous underwater vehicle safely reaches a target area.
Owner:HARBIN ENG UNIV

Wind-driven power generator yaw control method and module and control device based on control module

The invention discloses a wind-driven power generator yaw control method and module and a control device based on the control module, relates to the wind-driven power generator yaw control technology, and aims to solve the problem that the instantaneous wind direction interferes yaw control to allow a yaw unit to be started frequently, and unstable current output, difficulty in control and cabin service life lowering are caused. If wind speed exceeds a set value range or the deviation angle of the wind direction and a cabin is not larger than 16 degrees, the yaw unit keeps the state; if the deviation angle ranges between 16 degrees and 180 degrees, a yaw motor rotates reversely, or else the yaw motor rotates forwardly, and wind-driven power generator yaw control is achieved. The wind-driven power generator yaw control module is embedded into the control device based on the module. The yaw unit has a delay starting function and adopts error control, interference caused by the instantaneous wind speed is prevented, wind energy utilization rate is guaranteed, the situations of frequent starting and control difficulty caused by zero alignment are avoided, and cabin service life can be prolonged. The control method and module and the control device are applicable to wind-driven power generator yaw control.
Owner:STATE GRID CORP OF CHINA +1

Intelligent electric vehicle trajectory tracking and motion control method

The invention discloses an intelligent electric vehicle trajectory tracking and motion control method which comprises the following steps: judging whether a vehicle can work in a lateral stable rangeor not according to a given target trajectory and a current road condition; if the vehicle works in the stable area, executing the step 2; if the lateral stability range is exceeded, executing the step 3; 2, executing a working mode 1, and performing vehicle trajectory tracking and stability control by adopting vehicle trajectory tracking and yawing stability double closed-loop control: calculating an expected course angle of a vehicle according to an expected driving trajectory and a vehicle kinematics model; establishing a three-degree-of-freedom vehicle dynamic model, designing a trajectorytracking controller, inputting the difference between the expected course angle of the vehicle and the course angle of the previous moment into the trajectory tracking controller, and solving to obtain a front wheel rotation angle and a longitudinal speed; designing a yaw stability controller by adopting a model predictive control algorithm and then carrying out moment distribution; and 3, executing a working mode 2, and carrying out drifting control on vehicle trajectory tracking.
Owner:JILIN UNIV

Inertial navigation system

An inertial measurement system for a spinning projectile comprising: a first, roll gyro to be oriented substantially parallel to the spin axis of the projectile; a second gyro and a third gyro with axes arranged with respect to the roll gyro such that they define a three dimensional coordinate system; a controller, arranged to: compute a current projectile attitude from the outputs of the first, second and third gyros, the computed attitude comprising a roll angle, a pitch angle and a yaw angle; calculate a roll angle error based on the difference between the computed pitch and yaw angles and expected pitch and yaw angles; provide the roll angle error as an input to a Kalman filter that outputs a roll angle correction and a roll rate scale factor correction; and apply the calculated roll angle correction and roll rate scale factor correction to the output of the roll gyro; wherein the Kalman filter models roll angle error as a function of roll rate and one or more wind variables. The system provides improved calibration of the roll axis rate gyro scale factor, e.g. of an IMU fitted to a rolling projectile. A separate process (an Euler angle filter) is used to calculate an estimate of the roll angle error without the use of the Kalman filter and is then provided as an input to the Kalman filter which can then operate in a stable manner. The filter can be configured to estimate and correct for crosswind effects which would otherwise significantly degrade performance.
Owner:ATLANTIC INERTIAL SYST

Guidance method for attack time control

The invention discloses a guidance method for attack time control. The guidance method comprises the following steps of establishing mathematical models of a missile and a target by considering the three-dimensional space of motion of the missile and the target; obtaining a dynamic equation of the trajectory inclination angle and the trajectory deflection angle of the missile, and obtaining a dynamic equation of the distance between the missile and the target, the angle of sight of the missile and the deflection angle of sight of the missile; on the basis, establishing a dynamic equation of the attack time error of the missile; then, separately designing the guidance law of the missile according to a pitching channel and a yaw channel, wherein the guidance law of the pitching channel is designed as an augmented proportion guidance law, the guidance law of the yaw channel is designed as a guidance law with an attack time error feedback item, and the trajectory track is adjusted to realize time control over attack on the target; and when the yaw angle is zero, adjusting the guidance law of the yaw channel to avoid singularity conditions. According to the guidance method, the attack time error is estimated, the attack time error tends to be zero through a guidance strategy, and the distance between the missile and the target tends to be zero. The guidance method for attack time control has the characteristics of clear structure and high applicability.
Owner:BEIHANG UNIV

Aircraft overload tracking method taking overload and angular velocity as outer loop

ActiveCN111309042AEliminate overload static difference problemEliminate Insufficient Stability Margin ProblemsAttitude controlPosition/course control in three dimensionsGyroscopeAccelerometer
The invention relates to an aircraft overload tracking method taking overload and angular velocity as an outer loop, and belongs to the technical field of aircraft control. The method is characterizedin that an accelerometer is adopted to measure the actual overload of an aircraft; the actual overload is compared with an overload instruction to obtain an overload error; a gyroscope is adopted tomeasure a yaw rate, and nonlinear transformation is carried out to obtain two damping signals of an overload outer loop; and then two paths of integral signals are provided by the integral and nonlinear integral signals of the overload error; and finally, a proportional signal, the two paths of integral signals and the two paths of differential signals are integrated to form an overload error outer loop signal. And then integration and nonlinear integration are carried out on the outer ring signal, and the yaw rate signal is superposed to form an attitude stabilization loop of the overload inner ring instruction driven aircraft, so that a control target of lateral overload instruction tracking is realized. According to the method, overload control can be realized based on reserving of a traditional attitude loop.
Owner:NAVAL AVIATION UNIV

Steering redundancy and integrated control system and method of four-wheel independent driving electric automobile

The invention relates to a steering redundancy and integrated control system and method of a four-wheel independent driving electric automobile. The control method comprises the steps that a differential action power reference curve is determined by an automobile controller according to the steering wheel hand power demands of a driver; an electric power steering module obtains a power torque command according to the measured steering wheel rotating angle data and sends the power torque command to an EPS (Electronic Power Steering, electronic power steering system); a differential action powersteering module utilizes the differential action power reference curve to obtain a front axle differential action torque of the electric automobile according to the measured data; a reference yaw angle velocity is obtained according to the measured automobile practical yaw angle velocity, the steering wheel rotating angle and the automobile speed data, and accordingly the additive yawing moment is obtained; and the automobile controller utilizes the front axle differential action torque and the additive yawing moment to obtain a four-wheel driving motor target output torque. Compared with theprior art, the steering redundancy and integrated control system and method have the advantages that the individualized demands of the driver can be met, the driving safety of the automobile is improved, and the manipulation burden of the driver is relieved.
Owner:TONGJI UNIV
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