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Autonomous Guidance, Navigation, and Control of Spacecraft

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Spacecraft Dynamics and Control

Abstract

The autonomous guidance, navigation, and control (GNC) system is an essential component of a spacecraft. It serves the purposes of determining the attitude and orbital parameters of the spacecraft, guiding the spacecraft to move on the intended orbit or towards the desired target, and controlling the attitude and orbit of the spacecraft according to mission requirements without ground-station support.

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References

  1. Yuanjiu Lu (1993) Inertial sensors. China Astronautics Publishing House, Beijing

    Google Scholar 

  2. Wei Z (2008) Research on algorithm of sins and its realization. Harbin: Harbin Institute of Technology

    Google Scholar 

  3. Ren Z (1986) Autonomous satellite navigation and orbit-keeping using attitude sensors. J Astronaut

    Google Scholar 

  4. Guo J, Xie Y (2003) Attitude sensor based autonomous navigation research for GEO satellite. Aerosp Control 4

    Google Scholar 

  5. Liu J (2011) On the X-ray pulsar-based autonomous navigation methods for Spacecraft. Huazhong University of Science and Technology, Wuhan

    Google Scholar 

  6. Chu Y, Wang D, Xiong K et al (2012) Research on measurement time-delay compensation on X-ray pulsar-based navigation. J Astronaut 33(11):1617–1622

    Google Scholar 

  7. Zhou C, Qian W, Guo J et al (2015) Overview of pulsar-based navigation. J Nanjing Univ Inf Sci Technol (Natural Science Edition) 7(3)

    Google Scholar 

  8. Wang D, Wei C, Xiong K (2017) Autonomous navigation technology for spacecraft. National Defense Industry Press, Beijing

    Google Scholar 

  9. Wu H, Hu J, Xie Y (1990) Characteristic model-based intelligent adaptive control. National Defense Industry Press, Beijing

    Google Scholar 

  10. Xie Y, Zhang H, Jun Hu et al (2014) Automatic control system design of Shenzhou spacecraft for rendezvous and docking. Scientia Sinica Technologica 44(1):12–19

    Google Scholar 

  11. Yang J (2001) Orbital dynamics and control of spacecraft II. China Astronautic Publishing House, Beijing

    Google Scholar 

  12. Jun Hu (1998) All coefficients adaptive reentry lifting control of manned spacecraft. J Astronaut 19(1):9–13

    Google Scholar 

  13. Hu J, Zhang H (2014) Study on the reentry guidance for a manned Lunar return vehicle. Control Theory Appl 31(12): 1678–1685

    Google Scholar 

  14. Huang X, Zhang H, Wang D et al (2014) Autonomous navigation and guidance for Chang’e-3 soft landing. J Deep Space Exploration 1(1):52–59

    Google Scholar 

  15. Battin RH (1998) An Introduction to the mathematics and methods of astrodynamics, Revised Edition. AIAA Education Series, AIAA, Reston, VA

    Google Scholar 

  16. Liu L (2000) Orbit theory of spacecraft. National Defense Industry Press, Beijing

    Google Scholar 

  17. Szebehely Victor G (1967) Theory of orbits, the restricted problem of three bodies. Academic Press, New York and London

    Google Scholar 

  18. Sun Y, Zhou J (2008) Introduction to modern celestial mechanics. Higher Education Press, Beijing

    Google Scholar 

  19. Li J, Baoyin H (2007) Dynamics and control in deep space exploration. Mech Eng

    Google Scholar 

  20. Rayman MD (2003) The successful conclusion of the Deep Space 1 mission: important results without a flashy title. Space Technol 23(2/3):185–196

    Google Scholar 

  21. .Garner CE, Rayman MD (2014) In-flight operation of the Dawn ion propulsion system through year two of cruise to Ceres. In: The 50th AIAA/ASME/SAE/ASEE Joint propulsion conference

    Google Scholar 

  22. Kuninaka H, Shimizu Y, Yamada T et al (2005) Flight report during two years on HAYABUSA explorer propelled by microwave discharge ion engines. In: The 41st AIAA/ASME/SAE/ASEE Joint propulsion conference and exhibit

    Google Scholar 

  23. De Bruin J, Camino-Ramos O, Schoenmaekers J et al (2006) SMART-1 Lunar mission: operations close to Moon impact. In: Space Ops 2006 conference

    Google Scholar 

  24. Citron SJ, Dunin SE, Meissinger HF (1964) A terminal guidance technique for Lunar landing. AIAA J 2(3):503–509

    Google Scholar 

  25. Ingoldby RN (1978) Guidance and control system design of the Viking planetary lander. J Guidance Control 1(3):189–196

    Google Scholar 

  26. McInnes CR (1996) Nonlinear transformation methods for gravity-turn descent. J Guid Control Dyn 19(1):247–248

    Google Scholar 

  27. Wang D (2000) Guidance and control for lunar soft landing. Harbin Institute of Technology

    Google Scholar 

  28. Wang D, Li T, Ma X (2002) Optimal guidance for Lunar gravity-turn descent. Acta Automatica Sinica 28(3):385–390

    Google Scholar 

  29. Klumpp AR (1971) Apollo lunar-descent guidance, Charles Stark Draper Laboratory. R-695

    Google Scholar 

  30. Sostaric RR, Rea JR (2005) Powered descent guidance methods for the Moon and Mars. In: AIAA guidance, navigation, and control conference and exhibit. San Francisco, California, AIAA 2005–6287

    Google Scholar 

  31. Wang D, Li T, Yan H et al (2000) A sub-optimal fuel guidance law for Lunar soft landing. J Astronautics 21(4):55–63

    Google Scholar 

  32. Zhang H, Yifeng Guan X et al (2014) Guidance navigation and control for Chang'e-3 powered descent. Scientia Sinica Technologica 44(4): 377–384

    Google Scholar 

  33. Lee AY, Ely T, Sostaric R et al (2010) Preliminary design of the guidance, navigation, and control system of the Altair Lunar lander. In: AIAA guidance, navigation, and control conference. Toronto, Ontario, Canada, AIAA 2010–7717, pp 1–61

    Google Scholar 

  34. Topcu U, Casoliva J, Mease KD (2006) Fuel efficient powered descent guidance for Mars landing. In: AIAA guidance, navigation, and control conference and exhibit. San Francisco, California, AIAA 2005–6286

    Google Scholar 

  35. Springmann PN (2006) Lunar descent using sequential engine shutdown. Massachusetts Institute of Technology, Massachusetts

    Google Scholar 

  36. Mendeck GF, Carman GL (2002) Guidance design for Mars smart landers using the entry terminal point controller. In: AIAA atmospheric flight mechanics conference and exhibit. Monterey, California

    Google Scholar 

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Correspondence to Yongchun Xie .

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Xie, Y., Lei, Y., Guo, J., Meng, B. (2022). Autonomous Guidance, Navigation, and Control of Spacecraft. In: Spacecraft Dynamics and Control. Space Science and Technologies. Springer, Singapore. https://doi.org/10.1007/978-981-33-6448-6_7

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  • DOI: https://doi.org/10.1007/978-981-33-6448-6_7

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-33-6447-9

  • Online ISBN: 978-981-33-6448-6

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