Impact of Pseudo-Stochastic Pulse and Phase Center Variation on Precision Orbit Determination of Haiyang-2A from Experimental HY2 Receiver GPS Data

• Published in: Remote sensing (Basel, Switzerland) Switzerland), 2024-04, Vol.16 (8), p.1336
• Main Authors: Wang, Youyuan, Guo, Jinyun, Ya, Shaoshuai, Jia, Yongjun, Guo, Hengyang, Chang, Xiaotao, Liu, Xin
• Format: Article
• Language: English
• Subjects: Climate change; Data acquisition; Earth orbits; Global positioning systems; GPS; HY-2A; Kinematics; Low earth orbit satellites; Low earth orbits; Orbit determination; Performance evaluation; phase center variations; pseudo-stochastic pulse; reduced-dynamic orbit; satellite laser ranging; Satellite navigation systems; Satellite orbits; Satellites; Spatial data; Stochasticity
• ISSN: 2072-4292; 2072-4292
• DOI: 10.3390/rs16081336

Haiyang-2A (HY-2A) is the first marine dynamic environment satellite established by China, which has made significant contributions to the marine scientific research field. It carries the satellite-based GPS receiver named HY2, which was independently developed by China. It is an experimental satellite-borne GPS receiver for low earth orbit satellites, and during its operational period in orbit, the satellite-borne GPS data are not made accessible to the public. Therefore, this paper assesses the quality of HY-2A satellite-borne GPS data based on indicators such as satellite visibility, multipath effect, and ionospheric delay. The results indicate that the data acquired by the HY2 receiver are of high quality. The precise orbit determination (POD) uses the reduced-dynamic (RD) method. The adjustment effects of the pseudo-stochastic pulse time interval and a priori sigma on POD are analyzed, and the antenna phase center variation (PCV) is estimated using the direct method and residual method. Furthermore, this paper investigates the impact of PCV models with different resolutions (10° × 10° and 5° × 5°) on satellite orbit determination. To evaluate the orbit precision, three methods are used for validation, including carrier phase residual analysis, external precise science orbit (PSO) validation, and SLR three-dimensional (3D) validation, respectively. The results indicate that the highest orbit precision is achieved when the pseudo-stochastic pulse time interval is configured to 15 min, with the a priori sigma of 1 × 10−8 m/s2. The orbit carrier phase residuals reach the millimeter level. The 10° × 10°PCV model was estimated using the direct method and residual method, respectively; the root mean square of the external orbit validation for both methods show a millimeter-level improvement. The results obtained from the direct method and residual method are comparable. The resolution is increased from 10° to 5°, and the improvement in orbital precision is relatively small. The results obtained from the SLR 3D validation are consistent with those from the external PSO validation. The experimental results contribute valuable information for the POD of the HY2 series satellites.