An Experimental Study on Attitude Control of a Flexible Launch Vehicles Using Ground Testbed

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 333
  • Download : 0
Issue Date
2004-05-21
Language
KOR
Citation

제 5회 우주발사체기술 심포지움

URI
http://hdl.handle.net/10203/146447
Appears in Collection
AE-Conference Papers(학술회의논문)
Files in This Item
There are no files associated with this item.

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0