Abstract:The threat space of a satellite navigation signal distortion model describes the signal distortion range which causes a large differential error but is difficult to detect by receiver observations. The threat space may have disastrous consequences for civil aviation and other safety navigation services. A larger threat space increases the navigation services risk and the distortion detection requirements. Thus, satellite navigation systems need appropriate methods to minimize the threat space. This paper presents a method that reduces the range bias detection threshold to reduce the threat space. The effectiveness of this method is evaluated using the BeiDou Navigation Satellite System (BDS) B1C and B2a signals as examples. The results show that the threat space can be reduced by more than 40% compared to a space for a 20 m threshold when the ranging bias threshold is 5 m. This method should be implemented by using satellite onboard receivers to reduce the threat space.
[1] WONG G, PHELTS R E, WALTER T, et al. Characterization of signal deformations for GPS and WAAS satellites [C]//Proceedings of ION GNSS. San Diego, California: Institute of Navigation, 2010: 3143-3151. [2] International Civil Aviation Organization. ICAO international standards and recommended practices. Annex 10 to the convention on international civil aviation. Volume I radio navigation aids seventh edition: ISBN 978-92-9258-504-4[S]. Canada: International Civil Aviation Organization, 2018. [3] PAGOT J B. Modelling and monitoring of new GNSS signal distortions in the context of civil aviation [D]. Toulouse, France: Institute National Polytechnique de Toulouse (INPT), 2016. [4] PHELTS R E, WALTER T, ENGE P, et al. Signal deformation monitoring for dual-frequency WAAS [C]//Proceedings of ION ITM. San Diego, California: Institute of Navigation, 2013: 93-106. [5] WONG G, PHELTS R E, WALTER T, et al. Characterization of signal deformations for GPS and WAAS satellites [C]//Proceedings of ION GNSS. San Diego, California: Institute of Navigation, 2010: 3143-3151. [6] European Union. The Galileo open service signal in space interface control document (Issue 1.3): Galileo-OS-SIS-ICD-1.3[S]. Brussels: European Union, 2016. [7] 中国卫星导航系统管理办公室. 北斗卫星导航系统空间信号接口控制文件公开服务信号B1C(1.0版): BDS-SIS-ICD B1C-1.0[S]. 北京: 中国卫星导航系统管理办公室, 2017年. China Satellite Navigation Office. BeiDou Navigation Satellite System signal in space interface control document open service signal B1C (Version 1.0): BDS-SIS-ICD B1C-1.0[S]. Beijing: China Satellite Navigation Office, 2017. (in Chinese) [8] 中国卫星导航系统管理办公室. 北斗卫星导航系统空间信号接口控制文件公开服务信号B2a(1.0版): BDS-SIS-ICD B2a-1.0[S]. 北京: 中国卫星导航系统管理办公室, 2017年.China Satellite Navigation Office. BeiDou Navigation Satellite System signal in space interface control document open service signal B2a (Version 1.0): BDS-SIS-ICD B2a-1.0[S]. Beijing: China Satellite Navigation Office, 2017. (in Chinese) [9] LU M Q, LI W Y, YAO Z, et al. Overview of BDS Ⅲ new signals [J]. Navigation, 2019, 66(1): 19-35. [10] YAO Z, LU M, FENG Z M. Quadrature multiplexed BOC modulation for interoperable GNSS signals [J]. Electronics Letters, 2010, 46(17): 1234-1236. [11] YAO Z, LU M. Optimized modulation for compass B1-C signal with multiple processing modes [C]//Proceedings of ION GNSS 2011. Portland OR: Institute of Navigation, 2011: 19-23. [12] YAO Z, LU M. Constant envelope combination for components on different carrier frequencies with unequal power allocation [C]//Proceedings of ION ITM 2013. San Diego, California: Institute of Navigation, 2013: 629-637. [13] YAO Z, LU M. Dual-frequency constant envelope multiplex with non-equal power allocation for GNSS [J]. Electronics Letters, 2012, 48(25): 1624-1625.