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Design of nonlinear autopilots for high angle of attack missiles

Author(s):
Publication title:
AIAA paper
Title of ser.:
AIAA Paper : AIAA Guidance Navigation and Control Conference
Ser. no.:
1996
Pub. Year:
1996
No.:
96-3913
Paper no.:
96-3913
Page(from):
1
Page(to):
7
Pub. info.:
American Institute of Aeronautics and Astronautics
ISSN:
01463705
Language:
English
Call no.:
A07400
Type:
Technical Paper

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