Design and Validation of Flight Control Law Changes Intended to Minimize Pilot-Induced Oscillations in a Large Transport Aircraft
- 著者名:
- Shweyk, K. ( The Boeing Company, Long Beach, CA )
- Weltz, G.
- 掲載資料名:
- AIAA meeting papers on disc
- シリーズ名:
- AIAA Paper : AIAA Atmospheric Flight Mechanics Conference
- シリーズ巻号:
- 2005
- 発行年:
- 2005
- 通号:
- 2005-5812
- ペーパー番号:
- AIAA Paper 2005-5812
- 出版情報:
- [Reston, Va.]: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- 言語:
- 英語
- 請求記号:
- A07400/200516 [CD-ROM 2005 Disc 16]
- 資料種別:
- テクニカルペーパー
類似資料:
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
2
テクニカルペーパー
Adaptive/Reconfigurable Flight Control Augmentation Design Applied to High-Winged Transport Aircraft
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
9
テクニカルペーパー
Design and Flight Testing of Intelligent Flight Control Laws for the WVU YF-22 Model Aircraft
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
National Aeronautics and Space Adminstration |
6
テクニカルペーパー
Design, Development and Flight Testing of Control Laws for the Indian Light Combat Aircraft
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |