TY - JOUR
T1 - Low-Cost Onboard Multisensor State Estimator Based on Global Mixed Sampling Optimization Filter
AU - Liu, Xiaoxiong
AU - Wang, Yinglong
AU - Yang, Nan
AU - Yang, Yue
N1 - Publisher Copyright:
© 2001-2012 IEEE.
PY - 2023/7/1
Y1 - 2023/7/1
N2 - Long-term convergent and accurate state estimation (attitude, velocity, and position) is critical to unmanned aerial vehicles (UAVs). However, the measurement accuracy and noise of multiple low-cost sensors onboard are poorer compared with high-precision sensors. To improve the solution accuracy and reliability of UAVs' state estimation based on the low-cost sensors, a two-step multisensor fusion estimator [federated mixed sampling Kalman filter (FMSKF)] is proposed. First, a multisensor integrated navigation model array is designed depending on the different sensors, including the gyroscope, accelerometer, magnetometer, global positioning system (GPS) module, and barometer. Then, a three-stage mixed sampling Kalman filter is proposed to obtain the local convergent state vector, which is difficult to meet the flight accuracy requirements. Therefore, a multisensor global information optimization filter is proposed to obtain the global convergent navigation solution parameters. Finally, the simulation and flight experimental results and detailed analysis demonstrate that the proposed algorithm can improve the state estimation accuracy, filtering robustness, and obtain desirable navigation performance.
AB - Long-term convergent and accurate state estimation (attitude, velocity, and position) is critical to unmanned aerial vehicles (UAVs). However, the measurement accuracy and noise of multiple low-cost sensors onboard are poorer compared with high-precision sensors. To improve the solution accuracy and reliability of UAVs' state estimation based on the low-cost sensors, a two-step multisensor fusion estimator [federated mixed sampling Kalman filter (FMSKF)] is proposed. First, a multisensor integrated navigation model array is designed depending on the different sensors, including the gyroscope, accelerometer, magnetometer, global positioning system (GPS) module, and barometer. Then, a three-stage mixed sampling Kalman filter is proposed to obtain the local convergent state vector, which is difficult to meet the flight accuracy requirements. Therefore, a multisensor global information optimization filter is proposed to obtain the global convergent navigation solution parameters. Finally, the simulation and flight experimental results and detailed analysis demonstrate that the proposed algorithm can improve the state estimation accuracy, filtering robustness, and obtain desirable navigation performance.
KW - Global information optimization filter
KW - integrated navigation model array
KW - low-cost sensors
KW - mixed sampling Kalman filter
KW - multisensor fusion estimator
KW - state estimation
UR - http://www.scopus.com/inward/record.url?scp=85161026670&partnerID=8YFLogxK
U2 - 10.1109/JSEN.2023.3277483
DO - 10.1109/JSEN.2023.3277483
M3 - 文章
AN - SCOPUS:85161026670
SN - 1530-437X
VL - 23
SP - 14758
EP - 14772
JO - IEEE Sensors Journal
JF - IEEE Sensors Journal
IS - 13
ER -