The Landing Approach High Order System found that excessive delays between the pilot input and aircraft response could lead to a PIO.[1] It used the NT-33 variable stability aircraft.[1] The LAHOS study does not take into account non-linear effects.[2]
Sources
- [1] R. Loschke, “Development of the F-117 Flight Control System,” in AIAA Guidance, Navigation, and Control Conference and Exhibit, Austin, Texas: American Institute of Aeronautics and Astronautics, Aug. 2003. doi: 10.2514/6.2003-5762.
- [2] NATO, Ed., Flight Vehicle Integration Panel Workshop on Pilot Induced Oscillations: = (Atelier sur le Pompage Piloté). in AGARD advisory report, no. 335. Neuilly-sur-Seine: AGARD, 1995.
Backlinks
F-117 PIO
[[NT-33A]]
Pilot-Induced Oscillations