2016
DOI: 10.3390/s16122017
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MEMS IMU Error Mitigation Using Rotation Modulation Technique

Abstract: Micro-electro-mechanical-systems (MEMS) inertial measurement unit (IMU) outputs are corrupted by significant sensor errors. The navigation errors of a MEMS-based inertial navigation system will therefore accumulate very quickly over time. This requires aiding from other sensors such as Global Navigation Satellite Systems (GNSS). However, it will still remain a significant challenge in the presence of GNSS outages, which are typically in urban canopies. This paper proposed a rotary inertial navigation system (I… Show more

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Cited by 47 publications
(68 citation statements)
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“…The un‐converged estimates of d X and d Y indicate the low estimability of d E and d N , and so is the accelerometer biases γ X and γ Y . Due to the failed estimation of sensor biases, their modulation leads to the oscillating attitude errors , as shown in the figure. The only error state that can be estimated is γ Z .…”
Section: Estimability Analysis and Experimental Resultsmentioning
confidence: 98%
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“…The un‐converged estimates of d X and d Y indicate the low estimability of d E and d N , and so is the accelerometer biases γ X and γ Y . Due to the failed estimation of sensor biases, their modulation leads to the oscillating attitude errors , as shown in the figure. The only error state that can be estimated is γ Z .…”
Section: Estimability Analysis and Experimental Resultsmentioning
confidence: 98%
“…For the low‐cost MEMS IMUs, the gyro biases are usually much more significant than the ones in high‐end IMUs. For instance, the bias instability error for a MEMS IMU can be hundreds degrees per hour . Therefore, dE>>ωiecosLεU+ωiesinLgγE and dN>>ωiesinLgγN, which makes their estimability higher than other unobservable errors.…”
Section: Observability Analysis Of Inertial Systemsmentioning
confidence: 99%
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“…In the numerical simulation, both the GPS data and INS data contain errors. The error in terms of the GPS latitude, longitude and height is 10 m. To make this numerical simulation more challenging, we assume that the INS uses a low-precision MEMS gyroscope [26,27] and that the angle drift ratio is 20/h. In addition, we assume that the INS has been working for 60 s after the initial alignment.…”
Section: Numerical Simulation Resultsmentioning
confidence: 99%
“…It has also been studied in the low-cost MEMS IMUs in recent years [14,25]. From the frequency domain, there is a more intuitive understanding of the rotation modulation.…”
Section: Principle and Theoretical Modelmentioning
confidence: 99%