Wireless head tracker design method based on Kalman filtering and PPM coding
A Kalman filtering and design method technology, applied in position/direction control, control using feedback, TV, etc., can solve the problem of large error in three-way accelerometer measurement, achieve high precision, strong versatility, and light weight Effect
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Embodiment 1
[0045] This embodiment provides a wireless head tracking design method based on Kalman filtering and PPM coding, including the following steps:
[0046] Step 1: The camera on the aircraft terminal equipment first collects the image information and audio information in front of the drone or model aircraft, and transmits them to the user's head equipment in a wireless form through image transmission transmission;
[0047] Step 2: After receiving the image information and audio information transmitted by the drone, the image transmission in the user's head device outputs to the video glasses, and the video glasses present the received image and sound signals to the operator;
[0048] Step 3: The operator moves the head according to the initial screen sent back by the UAV or model aircraft, and combines the detection requirements. The nine-axis posture detection module on the user's head device senses the movement posture of the operator's head, and the main control board passes th...
Embodiment 2
[0060] This embodiment also provides an attitude angle estimation algorithm based on the Kalman filter, as follows:
[0061] According to the gravity component measured by the accelerometer under static conditions, the roll angle and pitch angle of the head of the carrier can be calculated according to formulas (1) and (2):
[0062] (1)
[0063] (2)
[0064] After the roll angle and pitch angle are calculated, the measured value of the magnetoresistive sensor is transformed once using formula (3):
[0065] (3)
[0066] According to formula (4), the yaw angle can be calculated by using the transformed magnetoresistive sensor data:
[0067] (4)
[0068]However, under dynamic conditions, it has unknown acceleration motion and vibration. At this time, the accelerometer must be affected by non-gravity acceleration. If the attitude angle is still calculated according to the above formula, there must be a large deviation between the result and the real value . Howev...
Embodiment 3
[0091] like figure 1 and figure 2 As shown: this embodiment also provides a wireless head-tracking system based on Kalman filtering and PPM coding, including user head equipment and aircraft end equipment, and the user head equipment includes video glasses, image transmission receiving, and master control board, a transmitter and a sensor board, the aircraft end equipment includes a receiver, a pan / tilt, a video transmission transmitter and a camera, the camera, a video transmission transmitter, a video transmission receiver and video glasses are connected in sequence, and the sensor, the main control board , the transmitter, the receiver and the pan / tilt are connected in sequence, and the camera is set on the pan / tilt.
[0092] The main control board includes a single-chip microcomputer chip.
[0093] The sensor board adopts a nine-axis attitude detection module, which includes a three-axis gyroscope, a three-axis digital accelerometer and a three-axis magnetoresistive sen...
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