13.5 Summary
461
propellant load, integrated ballast and propellant correction method, which gave a
solution to inertia measurement of the lunar lander, and improved test accuracy and
efficiency.
Professional metrology technology had played an important role in success of
the Chang’E-3 lunar lander. Along with continuous development of mission requirements, the accuracy, efficiency and reliability of professional metrology technology
will also be improved continuously.
References
1. Yan Z, Huang S (1998) Satellite manufacturing technology[M]. China Astronautic Publishing
House, Beijing
2. Huang G, Qin G (2007) Measurement methods of the large scale 3-D coordinate and its
system[J]. J Astronaut Metrol Meas 27(4):15–19
3. Wang H, Xu Z, Zhao K et al. (2011) Recent advances of mass property measuring technology
for spacecraft[J]. Spacecraft Environ Eng 28(2):171–174
4. Jianxin LIU, Guowei RUAN (2012) Comparative analyses of the measurement schemes for the
test of hang-staying, slow landing and obstacle-shunning of “CE” landing module[J]. Aerospace
Manuf Technol 1(6):34–41
5. Yang Z (2007) An analysis of measurement technology in spacecraft assembly[J]. Spacecraft
Environ Eng 24(6):390–392
6. Zhang H, Lin J, Zhu J (2012) Three-dimensional coordinate transformation accuracy and its
influencing factors[J]. Opto-Electron Eng 39(10):26–31
7. Zhou Na, An Zhiyong, Li Yonghao (2011) Large-sized three-dimensional profile measurement
technology based on laser radar[J]. Infrared and Laser Eng 40(12):2465–2468
8. Tao L, Yang Z, Ruan G et al. (2013) Alignment precision measurement method of satellite
engine based on laser radar[J]. Spacecraft Environ Eng 30(3):328–331
9. Yang Linghui, Yang Xueyou, Lao Dabao et al (2010) Large-scale coordinate measurement
method based on intersection of optical planes[J]. Infrared and Laser Eng 39(6):1105–1109
10. Chen Q, Sun G, Pang H et al. (2012). Large-size topography scanning with laser radar[J].
Spacecraft Environ Eng 29(2):215–219
11. Yan Z, Huang S (1997) A study of leakage detecting with mass spectrometry under non vacuum
environment[J]. Chin Space Sci Technol 17(5):41–45
12. Yan Zhiping, Huang Shuying (2001) A study of leakage detecting with mass spectrometry
under non vacuum environment[J]. Chin Space Sci Technol 21(3):42–46
13. Yan Z, Huang S (2002) Sensitivity estimation formula of leak detection method[J]. Chin Space
Sci Technol 22(1):59–64
14. Du C, Chen M (2004) Research on new test method of mass properties of spacecraft[J].
Spacecraft Environ Eng 21(3):11–15
15. Chen Mian, Du Chen (2005) New technology of celerity measure satellite 3 Axis Centre of
mass[J]. Spacecraft Environ Eng 22(6):358–359
461
propellant load, integrated ballast and propellant correction method, which gave a
solution to inertia measurement of the lunar lander, and improved test accuracy and
efficiency.
Professional metrology technology had played an important role in success of
the Chang’E-3 lunar lander. Along with continuous development of mission requirements, the accuracy, efficiency and reliability of professional metrology technology
will also be improved continuously.
References
1. Yan Z, Huang S (1998) Satellite manufacturing technology[M]. China Astronautic Publishing
House, Beijing
2. Huang G, Qin G (2007) Measurement methods of the large scale 3-D coordinate and its
system[J]. J Astronaut Metrol Meas 27(4):15–19
3. Wang H, Xu Z, Zhao K et al. (2011) Recent advances of mass property measuring technology
for spacecraft[J]. Spacecraft Environ Eng 28(2):171–174
4. Jianxin LIU, Guowei RUAN (2012) Comparative analyses of the measurement schemes for the
test of hang-staying, slow landing and obstacle-shunning of “CE” landing module[J]. Aerospace
Manuf Technol 1(6):34–41
5. Yang Z (2007) An analysis of measurement technology in spacecraft assembly[J]. Spacecraft
Environ Eng 24(6):390–392
6. Zhang H, Lin J, Zhu J (2012) Three-dimensional coordinate transformation accuracy and its
influencing factors[J]. Opto-Electron Eng 39(10):26–31
7. Zhou Na, An Zhiyong, Li Yonghao (2011) Large-sized three-dimensional profile measurement
technology based on laser radar[J]. Infrared and Laser Eng 40(12):2465–2468
8. Tao L, Yang Z, Ruan G et al. (2013) Alignment precision measurement method of satellite
engine based on laser radar[J]. Spacecraft Environ Eng 30(3):328–331
9. Yang Linghui, Yang Xueyou, Lao Dabao et al (2010) Large-scale coordinate measurement
method based on intersection of optical planes[J]. Infrared and Laser Eng 39(6):1105–1109
10. Chen Q, Sun G, Pang H et al. (2012). Large-size topography scanning with laser radar[J].
Spacecraft Environ Eng 29(2):215–219
11. Yan Z, Huang S (1997) A study of leakage detecting with mass spectrometry under non vacuum
environment[J]. Chin Space Sci Technol 17(5):41–45
12. Yan Zhiping, Huang Shuying (2001) A study of leakage detecting with mass spectrometry
under non vacuum environment[J]. Chin Space Sci Technol 21(3):42–46
13. Yan Z, Huang S (2002) Sensitivity estimation formula of leak detection method[J]. Chin Space
Sci Technol 22(1):59–64
14. Du C, Chen M (2004) Research on new test method of mass properties of spacecraft[J].
Spacecraft Environ Eng 21(3):11–15
15. Chen Mian, Du Chen (2005) New technology of celerity measure satellite 3 Axis Centre of
mass[J]. Spacecraft Environ Eng 22(6):358–359