Abstract
Shipboard landing of aircraft needs to acquire the real-time and precise relative position between shipboard and aircraft. If the technique of relative navigation based on differential carrier phase is used to solve the problem, the key point is fixing the ambiguity real-time and reliably. In general, wide lane carrier is used to solve the problem. At single epoch, the observable equations of double frequency wide lane carrier are ill-condition, so the code observable equations are needed to add in. Since the poor precision of the code pseudorange information, the ambiguity solved by it can’t reach the performance requirements in shipboard landing. A fitting method by selection of parameter weights is researched based on wide lane algorithm. The method estimates the two kinds of wide lane float ambiguities at first; then solves the individual ambiguity separately. It avoids the problems of poor precision from code equations. The calculation of experiment data shows that the algorithm can solve ambiguity reliably at single epoch and improve accuracy of relative position to centimeter level, which satisfies the requirements for shipboard landing of aircraft.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Li Y, Qiu Z (2008) Navigation and positioning, vol 537, 2nd edn. National Defence Industry Press, Beijing, pp 582–583
Tang D, Bi B, Wang X et al (2010) Summary on technology of automatic landing/carrier landing. J Chin Inertial Technol 18(5):550–555
Heo M, Pervan B, Gautier J et al (2004) Robust Airborne navigation algorithms for SRGPS. In: Proceedings of the IEEE
Niu F, Zhao J, Zhang Y et al (2010) Key principle and algorithms of JPALS. The 1st China satellite navigation conference, Bei Jing May 15–19
Pervan B, Chan F (2003) Performance analysis of carrier phase DGPS navigation for shipboard landing of aircraft. J Inst Navig 50(3):181–191
Rife J, Khanafseh S, Pullen S et al (2008) Navigation, interference suppression, and fault monitoring in the sea-based joint precision approach and landing system. Proc IEEE 96(12):1958–1975
Wang W, Gao C, Pan S (2012) Wide-lane ambiguity resolution of network RTK based on improved carrier phase smoothed pseudorange. Bull Surveying Mapp 4:41–46
Zhu H, Gao X, Bei J et al (2011) An algorithm of GPS ambiguity resolution on single-epoch. Sci Surveying Mapp 36(4):9–11
Yang R, Yuan Y, Ou J (2010) Real-time GNSS carrier phase differential technique for spacecraft rendezvous and docking. Scientia Sinica: Phys Mech Astron 40(5):651–657
Liu L (2005) The Research on the precise KINRTK theory and its applications. Wuhan University, Wuhan
Yang R, Ou J, Yuan Y et al (2006) Solving single-frequency phase ambiguity using parameter weights fitting and constrained equation ambiguity resolution methods. Cent South Univ Technol 13(1):93–98
Zhou Z, Yi J (1997) Principles and applications of GPS satellites surveying. Surveying and Mapping Press, Beijing, pp 123–124
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2013 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Li, B., Cao, K., Xu, J., Zhu, Y. (2013). Application of Carrier Phase Differential Relative Navigation for Shipboard Landing of Aircraft. In: Sun, J., Jiao, W., Wu, H., Shi, C. (eds) China Satellite Navigation Conference (CSNC) 2013 Proceedings. Lecture Notes in Electrical Engineering, vol 243. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-37398-5_18
Download citation
DOI: https://doi.org/10.1007/978-3-642-37398-5_18
Published:
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-37397-8
Online ISBN: 978-3-642-37398-5
eBook Packages: EngineeringEngineering (R0)