A simplified approach to nonlinear dynamic inversion based flight control
- 著者名:
- Smith, P.R. ( Flight Management and Control Department, Defence Evaluation and Research Agency, UK )
- 掲載資料名:
- A collection of technical papers : AIAA Atmospheric Flight Mechanics Conference and Exhibit, August 10-12, 1998/Boston, Massachusetts
- シリーズ名:
- AIAA Paper : AIAA Atmospheric Flight Mechanics Conference
- シリーズ巻号:
- CP9808
- 発行年:
- 1998
- 通号:
- 98-4461
- ペーパー番号:
- AIAA 98-4461
- 開始ページ:
- 762
- 終了ページ:
- 770
- 出版情報:
- Reston VA: American Institute of Aeronautics and Astronautics
- ISBN:
- 9781563472701 [1563472708]
- 言語:
- 英語
- 請求記号:
- A07400/9808
- 資料種別:
- テクニカルペーパー
類似資料:
1
テクニカルペーパー
Bifurcation analysis of a high incidence aircraft with nonlinear dynamic inversion control
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
2
テクニカルペーパー
Flight Control Reconfiguration based on Online Physical Model Identification and Nonlinear Dynamic Inversion
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
3
テクニカルペーパー
Flight Test Experience of a Non-linear Dynamic Inversion Control Law on the VAAC Harrier
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
10
テクニカルペーパー
Fault detection and isolation based on dynamic observers applied to gas turbine control sensors
The American Society of Mechanical Engineers |
5
テクニカルペーパー
Implementation of Pilot Commands in Aircraft Control: A New Approach Based on Dynamic Inversion
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
テクニカルペーパー
Dynamic Inversion via State Dependent Riccati Equation Approach: Application to Flight Vehicles
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |