Unmanned Aerial Vehicle Target Tracking Based on OTSCKF and Improved Coordinated Lateral Guidance Law
Bibliographic Data
| ID | 22034455 |
|---|---|
| Authors | Wei Jiang (0000-0002-0811-0648, Northwestern Polytechnical University), Jiang Wei (0009-0002-2497-2413, Northwestern Polytechnical University), Yongxi Lyu (0000-0001-8912-3418, Northwestern Polytechnical University, corresponding author), Jingping Shi (0000-0001-5700-2638, Shaanxi Province Key Laboratory of Flight Control and Simulation Technology, 1 Dongxiang Road, Chang’an District, Xi’an 710129, China) |
| Year | 2022 |
| Volume | 11 |
| Issue | 3 |
| Pages | 188 |
| Publication date | 2022-03-11 |
| Peer Reviewed | Yes |
| Open Access | Yes |
| Type | ARTICLE |
| Venue | ISPRS International Journal of Geo-Information (JOURNAL) |
| Journal identifiers | ISSN: 2220-9964 • E-ISSN: 2220-9964 |
| Publisher | MDPI AG (PUBLISHER • IT) |
| DOI | 10.3390/ijgi11030188 |
| OpenAlex | W4220884581 |
| Language | EN |
| References cited | 25 |
This paper proposes an approach of target tracking of a ground target for UAVs using Optimal Two-Stage Cubature Kalman Filter and Improved Coordinated Lateral Guidance Law. Firstly, the Optimal Two-Stage Cubature Kalman Filter (OTSCKF) is proposed to estimate the target motion. The OTSCKF combines two-stage filtering technology with CKF to improve the estimation accuracy. Secondly, to keep a constant distance between the UAV and the target, a new guidance law based on the lateral turning equation is proposed and its asymptotic stability is proven. On this basis, a distributed tracking algorithm is designed to balance the phase difference and achieve cooperation among multi-UAVs. Thirdly, numerical experiments are performed for the tracking problems of moving targets and the results verify the effectiveness of the proposed guidance algorithm
Kalman filter · Computer Science · Guidance and Control Systems · Mathematics · Robotics and Sensor-Based Localization · Target Tracking and Data Fusion in Sensor Networks · Artificial Intelligence
| Citation velocity | historical |
|---|---|
| Highly cited | No |