4.7 Article

Optimal Configuration Based on Lever Arm Effect Rejection Performance Index for Redundant Inertial Sensors

出版社

IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TIM.2021.3127629

关键词

Inertial sensors; Resource management; Performance analysis; Sensor systems; Measurement units; Measurement uncertainty; Gravity; Figure-of-merit (FOM); lever arm effect; optimal configuration; redundant sensors; symmetry allocation

资金

  1. Ministry of Science and ICT (MSIT), South Korea, through the Information Technology Research Center (ITRC) [IITP-2021-2018-0-01423]
  2. Unmanned Vehicle and SW Platform Research Program related to Public Procurement for Innovation - Ministry of Land, Infrastructure, and Transport (MOLIT) of Korea Government
  3. Korea Agency for Infrastructure Technology Advancement (KAIA) [21DPIW-C153340-03]

向作者/读者索取更多资源

Redundant inertial sensor systems can improve navigation performance and ensure fault detection or fault isolation functions. However, the enlargement of size may lead to unexpected side effects. The lever arm effect error can be minimized by carefully considering the configuration of redundant sensors, with the figure-of-merit (FOM) used as an indicator for obtaining the optimal configuration.
Redundant inertial sensor systems improve navigation performance and guarantee fault detection or fault isolation functions. However, they may cause unexpected side effects owing to their enlarged size. The misalignment between the center of gravity of the sensor system and the rotational origin of the vehicle results in the lever arm effect inducing significant acceleration errors. To minimize the lever arm effect error, the configuration of redundant sensors should be carefully considered, as their performance is highly dependent on its configuration. Thus, the figure-of-merit (FOM), which is considered a performance index or cost function, is proposed to obtain the optimal configuration for minimizing the lever arm effect error. Further, to define an FOM, the angular velocity and angular acceleration are considered as random variables and to quantify them, they were replaced as variances. The lever arm effect error was found to be completely eliminated when a redundant inertial measurement unit (RIMU) with more than eight single-axis inertial sensors was configured using the proposed FOM. Further, a case study and simulation were conducted to verify the proposed FOM and configuration, and it was found that the proposed FOM can be used to obtain the optimal configuration of the RIMU and as an indicator of the lever arm effect error.

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