2023
DOI: 10.3390/mi14061243
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The Tobit-Unscented-Kalman-Filter-Based Attitude Estimation Algorithm Using the Star Sensor and Inertial Gyro Combination

Abstract: For the orbit operation of spacecraft, due to environmental factors, a star sensor installed on the spacecraft must have data censoring, which greatly reduces the attitude determination ability of the traditional combined-attitude-determination algorithm. To address this problem, this paper proposes an algorithm for high-precision attitude estimation based on a Tobit unscented Kalman filter. This is on the basis of establishing the nonlinear state equation of the integrated star sensor and gyroscope navigation… Show more

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Cited by 3 publications
(3 citation statements)
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“…Because the monorail crane is a highly nonlinear system, both the driving state and outside noise can significantly affect how accurately the track slope can be recognized when traveling. Compared with the EKF algorithm, UKF can effectively filter out the interference of disturbance variables, improve the anti-interference ability of the system, and realize the precise identification of the monorail track slopes [31].…”
Section: Ukf Algorithmmentioning
confidence: 99%
“…Because the monorail crane is a highly nonlinear system, both the driving state and outside noise can significantly affect how accurately the track slope can be recognized when traveling. Compared with the EKF algorithm, UKF can effectively filter out the interference of disturbance variables, improve the anti-interference ability of the system, and realize the precise identification of the monorail track slopes [31].…”
Section: Ukf Algorithmmentioning
confidence: 99%
“…This approach contributes to enhancing the precision of the entire navigation system. When passing through a tunnel, although the signal is blocked and the information is inaccurate, the attitude information in the TMR digital compass is accurate and can continue to provide attitude correction for the [ 35 , 36 , 37 , 38 , 39 , 40 , 41 , 42 , 43 , 44 , 45 , 46 , 47 , 48 , 49 , 50 , 51 , 52 , 53 , 54 , 55 , 56 , 57 , 58 , 59 , 60 , 61 , 62 , 63 ].…”
Section: Design Of High-precision Portable Digital Compass Systemmentioning
confidence: 99%
“…However, the attitude update rate (AUR) of the traditional star sensor is usually 4–10 Hz, which is too low to accomplish navigation tasks independently. In order to improve the AUR, an integrated navigation system of a star sensor and inertial measurement unit (IMU) has become a kind of classic solution [ 23 , 24 , 25 , 26 , 27 , 28 , 29 ]. The attitude data of the star sensor have no drift but the update rate is low, while the update rate of the IMU is high, but the attitude data drift with time.…”
Section: Introductionmentioning
confidence: 99%