تقرير
Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations
| العنوان: | Boundary Avoidance Tracking for Instigating Pilot Induced Oscillations |
|---|---|
| المؤلفون: | Craun, Robert W, Acosta, Diana M, Beard, Steven D, Hardy, Gordon H, Leonard, Michael W, Weinstein, Michael |
| بيانات النشر: | United States: NASA Center for Aerospace Information (CASI), 2013. |
| سنة النشر: | 2013 |
| مصطلحات موضوعية: | Aircraft Stability And Control, Aircraft Design, Testing And Performance |
| الوصف: | In order to advance research in the area of pilot induced oscillations, a reliable method to create PIOs in a simulated environment is necessary. Using a boundary avoidance tracking task, researchers performing an evaluation of control systems were able to create PIO events in 42% of cases using a nominal aircraft, and 91% of cases using an aircraft with reduced actuator rate limits. The simulator evaluation took place in the NASA Ames Vertical Motion Simulator, a high-fidelity motion-based simulation facility. |
| نوع الوثيقة: | Report |
| اللغة: | English |
| URL الوصول: | https://ntrs.nasa.gov/citations/20140008294 |
| ملاحظات: | NNA08CG83C WBS 561581.02.08.01.46.02 NNA13AA07C |
| رقم الأكسشن: | edsnas.20140008294 |
| قاعدة البيانات: | NASA Technical Reports |
| الوصف غير متاح. |