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Variable structure-based nonlinear missile guidance/autopilot design with highly maneuverable actuators
Variable structure-based nonlinear missile guidance/autopilot design with highly maneuverable actuators
Detailed Information
- 자료유형
- 기사
- ISSN
- 10636536
- 저자명
- Fu-Kuang Yeh
- 서명/저자
- Variable structure-based nonlinear missile guidance/autopilot design with highly maneuverable actuators / Fu-Kuang Yeh , Kai-Yuan Cheng, Li-Chen Fu
- 발행사항
- New York, NY : Institute of Electrical and Electronics Engineers, 2004.
- 형태사항
- pp. 944-949
- 주기사항
- Indudes Bibiography Reference
- 원문정보
- url
- 모체레코드
- 모체정보확인
- Control Number
- kjul:60263495
MARC
008201016s2004 ai aa eng■022 ▼a10636536
■1001 ▼aFu-Kuang Yeh
■24510▼aVariable structure-based nonlinear missile guidance/autopilot design with highly maneuverable actuators▼dFu-Kuang Yeh▼e Kai-Yuan Cheng, Li-Chen Fu
■260 ▼aNew York, NY▼bInstitute of Electrical and Electronics Engineers▼c2004.
■300 ▼app. 944-949
■500 ▼aIndudes Bibiography Reference
■7001 ▼aKai-Yuan Cheng, Li-Chen Fu
■773 ▼tIEEE transactions on control systems technology▼gVol. 12 No. 6 (2004. 11)▼d2004, 11
■856 ▼uhttps://www.ieee.org
■SIS ▼aS029541▼b60077650▼h8▼s2▼fP
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