Full envelope missile longitudinal autopilot design using the state-dependent Riccati equation method
- Author(s):
- Mracek, Curtis P. ( Navigation and Control Branch, U.S. Air Force Armament Directorate )
- Cloutier, James R. ( Navigation and Control Branch, U.S. Air Force Armament Directorate )
- Publication title:
- A collection of technical papers : AIAA Guidance, Navigation and Control Conference, August 11-13, 1997, New Orleans, LA
- Title of ser.:
- AIAA Paper : AIAA Guidance Navigation and Control Conference
- Ser. no.:
- CP9710
- Pub. Year:
- 1997
- Vol.:
- Pt. 3
- No.:
- 97-3767
- Paper no.:
- AIAA-97-3767
- Page(from):
- 1697
- Page(to):
- 1705
- Pub. info.:
- Reston, VA: American Institute of Aeronautics and Astronautics
- ISBN:
- 9781563472343 [1563472341]
- Language:
- English
- Call no.:
- (pt.1)A07400/9710-1,(pt.2)A07400/9710-2,(pt.3)A07400/9710-3
- Type:
- Technical Paper
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