Output Feedback Adaptive Variable Structure Control of a Smart Projectile Fin

Output Feedback Adaptive Variable Structure Control of a Smart Projectile Fin

著者名:

S. Mani ( University of Nevada, Las Vegas, Las Vegas, NV )
S. Singh
W. Yim
A. Araujo ( Federal University of Rio Grande do Norte, Natal, Brazil )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Guidance Navigation and Control Conference

シリーズ巻号:

2006

発行年:

2006

通号:

2006-6326

ペーパー番号:

AIAA Paper 2006-6326

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200619 [CD-ROM 2006 Disc 19]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047246
シリーズID:	PA00000153
会議名:	AIAA Guidance, Navigation, and Control Conference and Exhibit
回次:	2006
会議開催地:	Keystone, Colorado
会議開催年:	2006.08.21-2006.08.24

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1 テクニカルペーパー Adaptive Control of a Projectile Fin Using Piezoelectric Elastic Beam Mani, S., Singh, S., Parimi, S., Yim, W., Trabia, M. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Output Feedback Form and Adaptive Control of a Nonlinear Aeroelastic System Singh, S., Wang, L. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Output feedback variable structure adaptive control of a flexible spacecraft Zeng, Yueming, Araujo, Aldayr D., Singh, Sahjendra N. American Institute of Aeronautics and Astronautics	8 国際会議録 Adaptive control of projectile fin angle using piezoelectric beam actuator Yim, W., Singh, S.N., Trabia, M.B. SPIE - The International Society of Optical Engineering
3 テクニカルペーパー Adaptive Output Feedback Control of a Nonlinear Aeroelastic Structure Xing,W., Singh,S. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Global Robust Control of Aeroelastic System Using Output Feedback K. Lee, S. Singh American Institute of Aeronautics and Astronautics
4 国際会議録 Direct adaptive control of a smart projectile fin by piezoelectric flexible beam actuator Mani, S., Singh, S. N., Parimi, S. K., Yim, W., Trabia, M. SPIE - The International Society of Optical Engineering	10 テクニカルペーパー Adaptive control of feedback linearizable nonlinear systems with application to flight control Singh, S., Steinberg, M. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Output feedback variable structure adaptive control of an aeroelastic system Zeng, Yueming, Singh, Sahjendra N. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Variable Structure Control of Unsteady Nonlinear Aeroelastic System with Partial State Information Gujjula, S., Singh, S. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Variable structure adaptive control of wing-rock motion of slender delta wings Araujo, Aldayr D. de, Singh, Sahjendra N. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Sliding mode output feedback control of a flexible rotor via magnetic bearings Lewis, A.S., Sinha, A., Wang, K.W. The American Society of Mechanical Engineers

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