484
14 Electrical Testing Technology of Lunar Lander
of Advanced Orbiting System (AOS), the ground test software shall be able to fully
and effectively verify the correctness of the virtual channel scheduling and packet
scheduling strategy. The design of complicated information flow, such as multi-probe
telecommunication and relay telecommunication [8], will result in higher requirements for the timeliness and integrity of test data acquisition, processing and storage.
And it is a brand new subject to test the nuclear power system in future deep space
probes [9], which make it necessary to develop the ground power supply equipment
that can replace and simulate the characteristics of the nuclear power supply. In term
of testing mode and process, multi-probe complex test is an important topic faced in
of deep space exploration. In addition, analysis and verification on test coverage of
complicated system shall be deeply researched, as well as the design and implementation of intelligent test and verification methodology. Along with development of
test technology, the theory and methodology of ground virtual test and verification
will also be introduced into the electrical test of deep space probes.
References
1. Robert M, Catherine L, Johan S et al (2002) SCOS-2000 MultiSat: the multi-satellite extension
of a mission controls system: SpaceOps. SpaceOps, USA
2. Marvin R (2005) NxTest and the development of synthetic instrumentation. Def Electron 2:6–10
3. Michael JS, David D (2003) ATE open system platform. IEEE-P1552 structured architecture
for test systems (SATS). IEEE, USA
4. Nestor P (2003) A vision for the future ESA Ground Operations Software: 16th Flight Dynamics
Workshop. 16th Flight Dynamics Workshop, USA
5. Wang Q (2008) Electrical test technology of spacecraft. China Science and Technology Press,
Beijing
6. Jong-oh P, Jong-yoen C et al (2002) Electrical Ground Support Equipment (EGSE) design for
small satellite. Astron Space Sci 19(3):215–224
7. Simons RN, Wintuchy EG (2011) Demonstration of multi-Gbps data rates at Ka-Band using
software-defined modem and broadband high power amplifier for space communications. Glenn
Research Center, USA
8. Jiao J, Yang Z, Zhou J et al (2011) Design of relay file delivery protocol in deep space
communication. J Spacecraft TT&C Technol 30(ZL):32–36
9. Cai S, He S (2004) Retrospect of development for radioisotope power systems in space and its
prospect of application in new century. Chin J Nuclear Sci Eng 24(2):97–104
14 Electrical Testing Technology of Lunar Lander
of Advanced Orbiting System (AOS), the ground test software shall be able to fully
and effectively verify the correctness of the virtual channel scheduling and packet
scheduling strategy. The design of complicated information flow, such as multi-probe
telecommunication and relay telecommunication [8], will result in higher requirements for the timeliness and integrity of test data acquisition, processing and storage.
And it is a brand new subject to test the nuclear power system in future deep space
probes [9], which make it necessary to develop the ground power supply equipment
that can replace and simulate the characteristics of the nuclear power supply. In term
of testing mode and process, multi-probe complex test is an important topic faced in
of deep space exploration. In addition, analysis and verification on test coverage of
complicated system shall be deeply researched, as well as the design and implementation of intelligent test and verification methodology. Along with development of
test technology, the theory and methodology of ground virtual test and verification
will also be introduced into the electrical test of deep space probes.
References
1. Robert M, Catherine L, Johan S et al (2002) SCOS-2000 MultiSat: the multi-satellite extension
of a mission controls system: SpaceOps. SpaceOps, USA
2. Marvin R (2005) NxTest and the development of synthetic instrumentation. Def Electron 2:6–10
3. Michael JS, David D (2003) ATE open system platform. IEEE-P1552 structured architecture
for test systems (SATS). IEEE, USA
4. Nestor P (2003) A vision for the future ESA Ground Operations Software: 16th Flight Dynamics
Workshop. 16th Flight Dynamics Workshop, USA
5. Wang Q (2008) Electrical test technology of spacecraft. China Science and Technology Press,
Beijing
6. Jong-oh P, Jong-yoen C et al (2002) Electrical Ground Support Equipment (EGSE) design for
small satellite. Astron Space Sci 19(3):215–224
7. Simons RN, Wintuchy EG (2011) Demonstration of multi-Gbps data rates at Ka-Band using
software-defined modem and broadband high power amplifier for space communications. Glenn
Research Center, USA
8. Jiao J, Yang Z, Zhou J et al (2011) Design of relay file delivery protocol in deep space
communication. J Spacecraft TT&C Technol 30(ZL):32–36
9. Cai S, He S (2004) Retrospect of development for radioisotope power systems in space and its
prospect of application in new century. Chin J Nuclear Sci Eng 24(2):97–104