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Modeling, Analysis, and Simulation of GPS Carrier Phase for Spacecraft Relative Navigation

  • Published:2007-11 Issue:6 Volume:30 Page:1628-1639
  • ISSN:0731-5090
  • Container-title:Journal of Guidance, Control, and Dynamics
  • language:en
  • Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Psiaki Mark L.1,Mohiuddin Shan1

Affiliation:

1. Cornell University, Ithaca, New York 14853-7501

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Cited by 56 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Relative Navigation Performance of LEO Vehicles Considering GPS–KPS Constellation and Measurement Characteristics;International Journal of Aeronautical and Space Sciences;2024-07-26

2. Precise Distributed Satellite Navigation: Differential GPS with Sensor-Coupling for Integer Ambiguity Resolution;2024 IEEE Aerospace Conference;2024-03-02

3. Demonstration of Single-Satellite GNSS Spoofer Geolocation;The International Technical Meeting of the The Institute of Navigation;2024-02-14

4. Low-Cost Inertial Aiding for Deep-Urban Tightly Coupled Multi-Antenna Precise GNSS;NAVIGATION: Journal of the Institute of Navigation;2023

5. Using PPP Information to Implement a Global Real-Time Virtual Network DGNSS Approach;IEEE Transactions on Vehicular Technology;2022-10
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