Zhou Weijing, Ye Jifei, Chang Hao, Li Nanlei. Simplified method for calculating semi-major axis under laser micro-thruster for nano-satellite[J]. Infrared and Laser Engineering, 2019, 48(S1): 120-125. doi: 10.3788/IRLA201947.S117008
| Citation:
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Zhou Weijing, Ye Jifei, Chang Hao, Li Nanlei. Simplified method for calculating semi-major axis under laser micro-thruster for nano-satellite[J]. Infrared and Laser Engineering, 2019, 48(S1): 120-125. doi: 10.3788/IRLA201947.S117008
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Simplified method for calculating semi-major axis under laser micro-thruster for nano-satellite
- 1.
State Key Laboratory of Laser Propulsion & Application,Department of Aerospace Science and Technology,Space Engineering University,Beijing 101416,China
- Received Date: 2018-11-12
- Rev Recd Date:
2018-12-22
- Publish Date:
2019-04-25
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Abstract
In order to solve the problem of orbit transfer of the nano-satellite under the action of micro-thrust of laser micro-thruster, a simplified semi-major axis calculation method for in-plane orbit transfer under the tangential thrust was proposed by using perturbation equation. The influence of the main perturbation factors such as the non-spherical perturbation, the atmospheric perturbation and solar pressure perturbation on the method was analyzed. And the orbital changes of the direct integration of the motion equation under various perturbations were compared with the results from the simplified method. The validity and application conditions of the simplified method was verified. The simulation results show that the orbit maneuverability for nano-satellites can be obtained by simplified calculation method under the tangential thrust of the order of 100N at orbital altitude above 300 km. What is more, for nano-satellite mission design stage, the solar pressure perturbation can be ignored, the atmospheric drag perturbation can be ignored above orbital altitude of 500 km, and the influence characteristics of non-spherical perturbation are similar to those of other satellites.
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References
|
[1]
|
Cao Xibin, Sun Zhaowei. Rapid Response Micro Satellite Design[M]. Beijing:Science Press, 2016:1. (in Chinese) |
|
[2]
|
Kang Guohua, Yang Binghui, Liu Yao, et al. The technology of light control based on small satellite formation[J]. Aerospace Control, 2018, 2:42-47, 82. (in Chinese) |
|
[3]
|
Qiao Yi, Li Xiaoyu, Zhao Tian. Analysis on typical military application of small satellite[J]. Foreign Electronic Measurement Technology, 2017, 36(3):47-50. (in Chinese) |
|
[4]
|
Wen Xin. The application status and development trend of satellite cluster system[J]. Frontiers, 2018, 12:80-91. (in Chinese) |
|
[5]
|
Tan Sheng, Wu Jianjun, Zhang Yu, et al. Research progress of laser-supported space micropropulsion technology[J]. Journal of Propulsion Technology, 2018, 11:2415-2428. (in Chinese) |
|
[6]
|
Ru Chengbo, Xu Jianbing, Dai Ji, et al. A summary of MEMS based solid propellant microthrusters(SPM) array[J]. Explosive Materials, 2016, 6:1-6. (in Chinese) |
|
[7]
|
Liu Jianzhong, Liang Daolun, Wang Yang, et al. Review on MEMS-based solid propellant micro-propulsion[J]. Nanotechnology and Precision Engineering, 2016, 14(1):48-54. (in Chinese) |
|
[8]
|
Lin Laixing. Micro-propulsion system for modern dmall datellites[J]. Spacecraft Engineering, 2010(6):13-20. (in Chinese) |
|
[9]
|
Hong Yanji, Wang Guangyu, Dou Zhiguo. State of art of laser ablation microthruster[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(9):1555-1564. (in Chinese) |
|
[10]
|
Hua Zuohao, Guo Ning, Mao Chengli, et al. Development situation of laser solid micro-thrust technique[J]. Chemical Propellants Polymeric Materials, 2018(1):13-18. |
|
[11]
|
Tang Guojian, Zhang Hongbo, Zhen Wei, et al. Dynamics and Control of Low-thrust Orbital Maneuver[M]. Beijing:Science Press, 2013:43. (in Chinese) |
|
[12]
|
Zhang Hongbo. Theories and Methods of Spacecraft Orbital Mechanics[M]. Beijing:National Defense Industry Press, 2015:61, 171, 221. (in Chinese) |
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