A New Optimal Nonlinear Control Method and its Application to Missile Guidance Law Design

A New Optimal Nonlinear Control Method and its Application to Missile Guidance Law Design

Author(s):

Publication title:

A collection of technical papers : AIAA Guidance, Navigation and Control Conference, Monterey, California, 5-8 August 2002

Title of ser.:

AIAA Paper : AIAA Guidance Navigation and Control Conference

Ser. no.:

2002

Pub. Year:

2002

Vol.:

Pt. 3

No.:

2002-5023

Paper no.:

AIAA-2002-5023

Page(from):

2319

Page(to):

2328

Pages:

10

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563475467 [1563475464]

Language:

English

Call no.:

A07400/024438 (Pt.3)

Type:

Technical Paper

Details

TDL ID:	ZA00001421
Series ID:	PA00000153
Conf. info. (Name):	AIAA Guidance, Navigation and Control Conference
Conf. info. (Number):	2002
Conf. info. (Venue):	Monterey, California
Conf. info. (Date):	2002.08.05-2002.08.08

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