Overhead maintenance robot combined attitude measurement method
A measurement method and robot technology, applied in the direction of measuring devices, navigation through speed/acceleration measurement, instruments, etc., can solve the problems of low precision, achieve the effect of improving accuracy, positioning and attitude determination
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Embodiment 1
[0033] Such as figure 1 As shown, the application provides a combined attitude measurement method of an overhead maintenance robot, including:
[0034] S100: Determine the satellite navigation observation model, and calculate the satellite navigation observations.
[0035] Specifically, such as figure 2 as shown,
[0036] S101: Determine three different satellite receiver position vectors, including: base station receiver vector, satellite receiver vector, and baseline lever arm vector.
[0037] S102: Extract pseudocode, carrier phase and Doppler frequency shift information from the output of the GNSS receiver;
[0038] S103: Taking double differences on the pseudocode, the carrier phase, and the Doppler frequency shift information respectively to obtain a pseudocode difference component, a carrier phase difference component, and a Doppler frequency shift difference component;
[0039] S104: Use the base station receiver vector, the satellite receiver vector, the baseline...
Embodiment 2
[0047] In order to reduce the impact of uncertain factors in GNSS raw data and further improve the accuracy of GNSS output results, this application also provides another combined attitude measurement method for overhead maintenance robots. The specific steps are as follows: image 3 Shown:
[0048] S100: Determine the satellite navigation observation model, and calculate the satellite navigation observations.
[0049] S200: Determine an observation model of the inertial navigation system, and obtain inertial navigation observations, where the inertial navigation observations include: angular velocity and acceleration.
[0050] Wherein, the acceleration information is obtained by calculating the lever-arm error of the antenna of the main GNSS receiver and the inertial sensor in the carrier coordinate system, the acceleration of gravity of the earth, and the angular rate of the earth's rotation. The angular velocity information is determined by the angular rate of the earth's ro...
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