Citation: | SONG Jian-mei, LI Quan-yun. Strapdown Homing Guidance System Design for Some Ammunition[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2006, 15(1): 43-47. |
[1] |
Williams E, Richman J, Friedland B. Design of an integr ated strapdow n g uidance and control system fo r a tactical missiles [R]. AIAA 83-2196, 1983.
|
[2] |
Que Zhiho ng, Liu Linke. The optimal design of a strapdow n terminal guidance system [J]. The Control Technology of Tactic Missile, 2002(2); 38-44. (in Chinese)
|
[3] |
Song Jianmei. Mo del r eference variable structure autopilot design for homing missile[J]. Journal of Beijing Institute of Technology, 2001, 10(4); 364-369.
|
[4] |
Song Jianmei. Variable structure proport ional nav igationfor homing missile [J]. Journal of Beijing Institute ofT echnolog y, 2000, 9(3); 296-301.
|
[5] |
Zhou Donghua, Ye Yingzong. The technology of modernfault diagnosis and faulttoler ant[M]. Beijing; Tsing huaUniversity Press, 2000. (in Chinese)
|
[6] |
Song Jianmei. Passive homing missile?? s variable structurepropor tional navigation w ith terminal angular constraint[J]. Chinese Journal of Aeronautics, 2001, 14(2); 83-87.
|