GPS-based satellite formation flight simulation and applications to ionospheric remote sensing

REFERENCES

1. 1.↵
   1. Bandyopadhyay S,
   2. Foust R,
   3. Subramanian GP,
   4. Chung SJ,
   5. Hadaegh FY

   . Review of formation flying and constellation missions using nanosatellites. Journal of Spacecraft and Rockets. 2016;567-578.
2. 2.↵
   1. Escoubet CP,
   2. Schmidt R,
   3. Goldstein ML

   . Cluster-science and mission overview. In: The Cluster and Phoenix Missions. Dordrecht: Springer; 1997:11-32.
3. 3.↵
   1. Curtis S

   . The magnetospheric multiscale mission … resolving fundamental processes in space plasmas. Technical Report. 1999:1-56.
4. 4.↵
   1. Tapley BD,
   2. Bettadpur S,
   3. Ries JC,
   4. Thompson PF,
   5. Watkins M

   . GRACE measurements of mass variability in the Earth system. Science. 2004;305(5683):503-505.

   Abstract/FREE Full Text
5. 5.↵
   1. Friis-Christensen E,
   2. Lühr H,
   3. Knudsen D,
   4. Haagmans R

   . Swarm—an Earth observation mission investigating geospacer. Advances in Space Research. 2008;41(1):210-216.

   CrossRefWeb of Science
6. 6.↵
   1. Alfriend KT,
   2. Vadali SR,
   3. Gurfil P,
   4. How JP,
   5. Berger LS

   . Spacecraft Formation Flying: Dynamics, Control and Navigation. UK: Elsevier; 2010.
7. 7.↵
   1. Anthes RA,
   2. Bernhardt PA,
   3. Chen Y, et al

   . The COSMIC/-FORMOSAT-3 mission: early results. Bulletin of the American Meteorological Society. 2008;89(3):313-333.

   CrossRefWeb of Science
8. 8.↵
   1. Kelley MC

   . The Earth’s Ionosphere: Plasma Physics and Electrodynamics. 96 Academic Press; 2009.
9. 9.↵
   1. Kintner PM,
   2. Psiaki M,
   3. Humphreys T, et al.

   A Beginner’s Guide to Space Weather and GPS. Lecture Notes. 2008.
10. 10.↵
    1. Leitner J

    . A hardware-in-the-loop testbed for spacecraft formation flying applications. IEEE Aerospace Conference Big Sky, MT; 2001;2:615.
11. 11.↵
    1. Busse FD,
    2. How JP,
    3. Simpson J

    . Demonstration of adaptive extended Kalman filter for low earth orbit formation estimation using CDGPS. NAVIGATION. 2003;50:79-93.
12. 12.↵
    1. Burns R,
    2. Naasz B,
    3. Gaylor D,
    4. Higinbotham J

    . An environment for hardware-in-the-loop formation navigation and control. AIAA/AAS Astrodynamics Specialist Conference and Exhibit. 2004; Providence, USA:4735.
13. 13.↵
    1. Mohiuddin S,
    2. Psiaki ML

    . Satellite relative navigation using carrier-phase Differential GPS with integer ambiguities. AIAA Guidance, Navigation, and Control Conference and Exhibit. 2005; San Francisco, CA:6054.
14. 14.↵
    1. Gill E,
    2. Naasz B,
    3. Ebinuma T

    . First results from a hardware-in-the-loop demonstration of closed-loop autonomous formation flying. 26th Annual AAS Guidance and Control Conference. 2003; Breckenridge, CO.
15. 15.↵
    1. Leung S,
    2. Montenbruck O

    . Real-time navigation of formation-flying spacecraft using global positioning system measurements. Journal of Guidance, Control, and Dynamics. 2005;28(2):226-235.

    CrossRef
16. 16.↵
    1. Yamamoto T,
    2. D’Amico S

    . Hardware-in-the-loop demonstration of GPS-based autonomous formation flying. NAVITEC. 2008; Noordwijk, Netherlands.
17. 17.↵
    1. Marji Q

    . Precise Relative Navigation for Satellite Formation Flying Using GPS. Master Thesis. University of Calgary, Canada; 2008.
18. 18.↵
    1. Eyer JK

    . A Dynamics and Control Algorithm for Low Earth Orbit Precision Formation Flying Satellites. Ph.D. Dissertation. University of Toronto, Canada; 2009.
19. 19.↵
    1. Eddy D,
    2. Giralo V,
    3. D’Amico S

    . Development and verification of the Stanford GNSS navigation testbed for spacecraft formation-flying. Technical Note. 2017.
20. 20.↵
    1. Park JI,
    2. Park HE,
    3. Park SY,
    4. Choi KH

    . Hardware-in-the-loop simulations of GPS-based navigation and control for satellite formation flying. Advances in Space Research. 2010;46(11): 1451-1465.
21. 21.↵
    1. Vallado DA

    . Fundamentals of Astrodynamics and Applications. 4th ed. Springer Science & Business Media; 2001.
22. 22.↵
    1. Montenbruck O,
    2. Gill E

    . Satellite Orbits. Heidelberg, Germany: Springer-Verlag; 2001.
23. 23.↵
    1. Jones KG

    . Vehicle reference frames and vehicle motion handling in SimGEN (PC) software. Spirent Communication plc. Technical Report. DGP01062AAA. 2011.
24. 24.↵
    1. Yaakov BS,
    2. Li XR,
    3. Thiagalingam K

    . Estimation with Applications to Tracking and Navigation. New York; Johh Wiley and Sons; 2001.
25. 25.↵
    1. Cloutier JR

    . State-dependent Riccati equation techniques: an overview. IEEE American Control Conference. 1997;2:923-936.
26. 26.↵
    1. Gaposchkin EM,
    2. Coster AJ

    . GPS L1-L2 bias determination. Technical Report 971. MIT Lincoln Laboratory; 1993.
27. 27.↵
    1. Rideout W,
    2. Coster A

    . Automated GPS processing for global total electron content data. GPS Solutions. 2006;10(3):219-228.
28. 28.↵
    1. Peng Y

    . GNSS-based Spacecraft Formation Flying Simulation and Ionospheric Remote Sensing Applications. Master Thesis. Virginia Polytechnic Institute and State University; 2017.
29. 29.↵
    1. Rodrigues FS,
    2. De Paula ER,
    3. Abdu MA, et al

    . Equatorial spread F irregularity characteristics over Sao Luis, Brazil, using VHF radar and GPS scintillation techniques. Radio Science. 2004;39 (1):1-9.
30. 30.↵
    1. Richmond AD,
    2. Ridley EC,
    3. Roble RG

    . A thermosphere/ionosphere general circulation model with coupled electrodynamics. Geophysical Research Letters. 1992;19(6):601-604.
31. 31.↵
    1. Xu D,
    2. Morton Y,
    3. Jiao Y,
    4. Rino C

    . Simulation and tracking algorithm evaluation for scintillation signals on LEO satellites traveling inside the ionosphere. IEEE/ION PLANS 2018. Monterey, CA; April 2018:1143-1150.
32. 32.↵
    1. Forte B,
    2. Aquino M,
    3. Elmas ZG,
    4. Vadakke SV

    . On the use of the of the Cornell Scintillation Model within a Spirent signal simulator for the simulation of ionospheric scintillation events. International Ionospheric Effects Symposium (IES2011). 2011; Alexandria, VA.
33. 33.↵
    1. Rino CL,
    2. Tsunoda RT,
    3. Petriceks J,
    4. Livingston RC,
    5. Kelley MC,
    6. Baker KD

    . Simultaneous rocket-borne beacon and in situ measurements of equatorial spread F—intermediate wavelength results. Journal of Geophysical Research: Space Physics. 1981;86 (A4):2411-2420.