Configuration Parameter Design for ADAM-type Articulated Mast Based on Maximizing Specific Stiffness

doi:10.3780/j.issn.1000-758X.2013.04.007

Abstract

Abstract: The performances of the ADAM-type mast, such as mass, packaging size, stiffness and strength, are determined by its configuration parameters. A new design of configuration parameters based on maximizing specific stiffness was presented. By MATLAB and ANSYS joint simulation，the varying of specific stiffness with different configuration parameters was analyzed. The simulation results show that the optimum value of the length ratio of longeron to batten and the canister radius increases with the increase of the length of mast, when the length of ADAM-type varies in the range of 20 to 100 meters. While the length of mast is 20, 60, and 100 meters, the optimum value of the canister radius varies from 0.3 to 0.4 meter, 0.5 to 0.7 meter and 0.6 to 0.9 meter respectively. The design flow of configuration parameter based on maximizing specific stiffness is as follow: the canister radius is settled at first, then the length ratio of longeron to batten should be determined, and the number of longitudinal member could be finally settled. By this method, configuration parameters of the mast in the SRTM program are designed, and the results approximate to that of ADAM′s.

Key words: Able deployable articulated mast, Specific stiffness, Configuration, Modal analysis, Optimization, Spacecraft

LI Biao, CHENG Gang, LIU Zhi-Quan, DING Feng. Configuration Parameter Design for ADAM-type Articulated Mast Based on Maximizing Specific Stiffness[J]. Chinese Space Science and Technology, 2013, 33(4): 47-54.

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2013.04.007

https://journal26.magtechjournal.com/kjkxjs/EN/Y2013/V33/I4/47

[1]	MENG Henghui, XU Yawei, HAN Dongyang, LIU Xin, GENG Liyin, ZHANG Qingjun, LIU Liping, ZHANG Hongxing, WANG Yuying. Design and verification of loop heat pipe coupling heat system based on brazing technology [J]. Chinese Space Science and Technology, 2024, 44(5): 57-65.
[2]	ZHENG Xinyu, ZHANG Yi, ZHOU Jie, TANG Peijia, PENG Shengren, DANG Zhaohui. Improvement and application of MCTS in turn-based orbital games [J]. Chinese Space Science and Technology, 2024, 44(5): 75-82.
[3]	LI Ruifeng, SUN Chong, WANG Zheng, FANG Qun, ZHANG Xiang. Capture configuration design for space non-cooperative target based on reachable domain [J]. Chinese Space Science and Technology, 2024, 44(5): 83-94.
[4]	LI Ruixuan, LI Feng, XIN Lei, LU Xiaotian, LIU Feng. Video satellite image stabilization method based on maritime multi-targets [J]. Chinese Space Science and Technology, 2024, 44(5): 136-146.
[5]	GUO Yanning, LI Gaojian, YU Yongbin. Multi-impulse pursuit-evasion game in GEO based on improved dung beetle optimization [J]. Chinese Space Science and Technology, 2024, 44(4): 1-10.
[6]	WANG Jie, ZHONG Zikai, YUAN Hao, SONG Haibo. Orbit optimization for an asteroid-defense spacecraft departing from large elliptical parking orbit [J]. Chinese Space Science and Technology, 2024, 44(4): 102-110.
[7]	TAO Xinyong, KANG Guohua, WU Junfeng, HU Miaomiao, YANG Zhenghao, ZHOU Shaohui. Design of flexible docking mechanism for micro-nano satellites [J]. Chinese Space Science and Technology, 2024, 44(4): 119-129.
[8]	WANG Yazhou, DIAN Songyi, XIANG Guofei. A deep neural network assisted trajectory optimization algorithm for vertical landing vehicles [J]. Chinese Space Science and Technology, 2024, 44(4): 130-141.
[9]	CHEN Shiyu, NI Yanshuo, PENG Jing. Orbit design method of near-lunar space constellation [J]. Chinese Space Science and Technology, 2024, 44(3): 15-29.
[10]	LEI Yongjun, LU Dongning, YUAN li, CHEN chao. An attitude control method of satellites with hybrid flywheel configuration for skew maneuvers [J]. Chinese Space Science and Technology, 2024, 44(3): 111-119.
[11]	JIANG Yipeng, CUI Yufu, LIU Zhijia, QING Jiang. Optimization of drag reduction configuration on windward side of very low orbit spacecraft [J]. Chinese Space Science and Technology, 2024, 44(3): 120-126.
[12]	ZHOU Siyu, GU Yingying, YANG Yuetang, SHI Liheng, MA Yuxuan, ZHU Feihu, ZHANG Yunfang, WU Guanhao. Space application and test design of dual-comb ranging technique [J]. Chinese Space Science and Technology, 2024, 44(3): 127-135.
[13]	TIAN Dake, SONG Yuqun, JIN Lu, GAO Haiming, LIU Rongqiang, ZHAO Bingfeng. Design and analysis of radiating rib space deployable antenna mechanism [J]. Chinese Space Science and Technology, 2024, 44(2): 40-50.
[14]	GAO Xin, NIAN Jiawei, LIU Hongjin, YANG Mengfei. Efficient cache replacement framework based on access hotness for spacecraft processors [J]. Chinese Space Science and Technology, 2024, 44(2): 74-88.
[15]	HUANG Yuan, WEI Chunling, YAN Han, HAO Renjian. Ability modeling for spacecraft control system based on partial least square structural equation model approach [J]. Chinese Space Science and Technology, 2024, 44(2): 98-108.

Configuration Parameter Design for ADAM-type Articulated Mast Based on Maximizing Specific Stiffness

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments