执行机构驱动单元软件的设计与分析

doi:10.3969/j.issn.1674-1579.2015.05.011

Abstract

Abstract: The design procedure of ADU（actuator drive unit）software is introduced. The outer and inner time sequence restriction, such as 1553B message order and critical resource accessing order, are analyzed. The valid confirmation is presented. On software reliability, the key variables or system parts are recognized by SFMEA(software failure modes and effects analysis). Protection of singleevent upset of them is given. The validation of protection measure is validated.

Key words: actuator drive unit, time sequence, 1553B, interrupt, SEU

CLC Number:

TP311

ZHAO Xing-Song, DONG Xiao-Gang, YANG Xiao-Long, NIU He-Ming, GAO Meng. Design and Analysis of ADU Software[J]., 2015, 41(5): 53-.

0
/ / Recommend

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

URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2015.05.011

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2015/V41/I5/53

[1]	HUANG Yusong, TIAN Dong, Li Hongjue, JIAO Ronghui, LI Fei. A Trajectory Planning and Tracking Algorithm for the Tumbling Non Cooperative Spacecraft Approach, Flying around and Obstacle Avoidance [J]. Aerospace Contrd and Application, 2021, 47(3): 1-8.
[2]	CHEN Rui, YU Tingting, JIA Chunpeng, LI Chao, GAO Dongdong, JIANG Yunsong. OutofBounds Array Access Bug Characteristics in Aerospace Embedded Software [J]. Aerospace Contrd and Application, 2021, 47(2): 1-9.
[3]	Design of B Data Bus Protocol Based on ECSS for Spacecraft Attitude and Orbit Control System. Design of 1553B Data Bus Protocol Based on ECSS for Spacecraft Attitude and Orbit Control System [J]. Aerospace Contrd and Application, 2020, 46(2): 41-48.
[4]	JIN Yi-Huan, LEI Ye-Hong, FENG Hao, PENG Ji-Ping, TIAN Ye. Guidance Law Design for AirtoAir Missile Overthe Shoulder Based on Virtual Target [J]. , 2018, 44(3): 15-21.
[5]	ZHOU Yu-Kui, YANG Hua, QIAO Lei. Formal Modeling and Verification Method of InterruptManagement Requirement and Design Based on EventB [J]. , 2017, 43(3): 71-78.
[6]	ZHANG Pei-Jun, LIU Lu-Hua, WANG Jian-Hua. Optimal Ascent Trajectory Design for SingleStagetoOrbit Space Planes Based on Gauss Pseudospectral Method [J]. , 2017, 43(2): 13-20.
[7]	WANG Wei, GUO Hui-Jie, MENG Yue. Design on Configuration Schemes of Satellite/Pseudolite Integrated Navigation System [J]. , 2016, 42(3): 27-32.
[8]	WANG Huan-Jie, JIN Lei, JIA Ying-Hong. Agile Satellite Attitude Maneuver Control Using Hybrid Actuators [J]. , 2015, 41(6): 19-.
[9]	PENG Kun. One Kind of PseudoRate Modulator Based on Digital Integrated FPGA [J]. , 2015, 41(4): 49-53.
[10]	HOU Cheng-Jie. Interrupt Resource Conflict Analysis for Spacecraft C51 Language Software [J]. , 2015, 41(4): 58-62.
[11]	SUN Shuai, LI Zhi-Bin- , TIAN Ke-Feng. Modeling and Trajectory Planning of Return Process for a Class of Airship with Wind Field [J]. , 2014, 40(4): 37-41.
[12]	WANG Ruo-Chuan, YANG Meng-Fei, QIAO Lei. Modeling and Verification of Operating System Interrupt Management Based on Timed Automata [J]. , 2014, 40(4): 52-56.

Design and Analysis of ADU Software

PDF (PC)

Like

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 12

Metrics

Comments

Recommended 0