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Items: 7

1.

A Novel Rotation Scheme for MEMS IMU Error Mitigation Based on a Missile-Borne Rotation Semi-Strapdown Inertial Navigation System.

Jing Z, Li J, Zhang X, Feng K, Zheng T.

Sensors (Basel). 2019 Apr 9;19(7). pii: E1683. doi: 10.3390/s19071683.

2.

Reference markers of bone turnover for prediction of fracture: a meta-analysis.

Tian A, Ma J, Feng K, Liu Z, Chen L, Jia H, Ma X.

J Orthop Surg Res. 2019 Feb 28;14(1):68. doi: 10.1186/s13018-019-1100-6. Review.

3.

The Optimal Design of Modulation Angular Rate for MEMS-Based Rotary Semi-SINS.

Zhang J, Li J, Che X, Zhang X, Hu C, Feng K, Xu T.

Micromachines (Basel). 2019 Feb 10;10(2). pii: E111. doi: 10.3390/mi10020111.

4.

An Improved Strong Tracking Cubature Kalman Filter for GPS/INS Integrated Navigation Systems.

Feng K, Li J, Zhang X, Zhang X, Shen C, Cao H, Yang Y, Liu J.

Sensors (Basel). 2018 Jun 12;18(6). pii: E1919. doi: 10.3390/s18061919.

5.

Analysis and Compensation of Modulation Angular Rate Error Based on Missile-Borne Rotation Semi-Strapdown Inertial Navigation System.

Zhang J, Li J, Zhang X, Che X, Huang Y, Feng K.

Sensors (Basel). 2018 May 4;18(5). pii: E1430. doi: 10.3390/s18051430.

6.

Correction: A New Quaternion-Based Kalman Filter for Real-Time Attitude Estimation Using the Two-Step Geometrically-Intuitive Correction Algorithm. Sensors 2017, 17, 2146.

Feng K, Li J, Zhang X, Shen C, Bi Y, Zheng T, Liu J.

Sensors (Basel). 2017 Nov 3;17(11). pii: E2530. doi: 10.3390/s17112530.

7.

A New Quaternion-Based Kalman Filter for Real-Time Attitude Estimation Using the Two-Step Geometrically-Intuitive Correction Algorithm.

Feng K, Li J, Zhang X, Shen C, Bi Y, Zheng T, Liu J.

Sensors (Basel). 2017 Sep 19;17(9). pii: E2146. doi: 10.3390/s17092146. Erratum in: Sensors (Basel). 2017 Nov 03;17 (11):.

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