Missile Autopilot Design Using a New Suboptimal Nonlinear Control Method.

Missile Autopilot Design Using a New Suboptimal Nonlinear Control Method.

Author(s):

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2003

Pub. Year:

2003

No.:

2003-0577

Paper no.:

2003-0577

Pages:

9

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001712
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	41st
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2003.01.06-2003.01.09
Note for article:	41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 6-9 January 2003

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