原文传递
A Flight Control System Architecture for the NASA AirSTAR Flight Test Infrastructure
| 题名： | A Flight Control System Architecture for the NASA AirSTAR Flight Test Infrastructure |
| 作者： | Murch, Austin M. |
| 关键词： | architecture；structure；control；light；airs；nasa；star；flig；irst；system |
| 摘要： | A flight control system architecture for the NASA AirSTAR infrastructure has been designed to address the challenges associated with safe and efficient flight testing of research control laws in adverse flight conditions. The AirSTAR flight control system provides a flexible framework that enables NASA Aviation Safety Program research objectives, and includes the ability to rapidly integrate and test research control laws, emulate component or sensor failures, inject automated control surface perturbations, and provide a baseline control law for comparison to research control laws and to increase operational efficiency. The current baseline control law uses an angle of attack command augmentation system for the pitch axis and simple stability augmentation for the roll and yaw axes. |
| 报告类型： | 科技报告 |
相关文献
- Practical Application of a Subscale Transport Aircraft for Flight Research in Control Upset and Failure Conditions
- Subscale Flight Testing for Aircraft Loss of Control: Accomplishments and Future Directions.
- Subscale Flight Testing for Aircraft Loss of Control: Accomplishments and Future Directions.
- AirSTAR A UAV Platform for Flight Dynamics and Control System Testing
- UAS Integration in the NAS Project Flight Test Planning Status.
- Current and Future Research in Active Control of Lightweight, Flexible Structures Using the X-56 Aircraft.
检索历史
应用推荐
