Full envelope missile longitudinal autopilot design using the state-dependent Riccati equation method

Full envelope missile longitudinal autopilot design using the state-dependent Riccati equation method

著者名:

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 )

掲載資料名:

A collection of technical papers : AIAA Guidance, Navigation and Control Conference, August 11-13, 1997, New Orleans, LA

シリーズ名:

AIAA Paper : AIAA Guidance Navigation and Control Conference

シリーズ巻号:

CP9710

発行年:

1997

巻:

Pt. 3

通号:

97-3767

ペーパー番号:

AIAA-97-3767

開始ページ:

1697

終了ページ:

1705

出版情報:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563472343 [1563472341]

言語:

英語

請求記号:

(pt.1)A07400/9710-1,(pt.2)A07400/9710-2,(pt.3)A07400/9710-3

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00005891
シリーズID:	PA00000153
会議名:	AIAA Guidance, Navigation and Control Conference
回次:	1997
会議開催地:	New Orleans, LA
会議開催年:	1997.08.11-1997.08.13

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