TY - GEN
T1 - Integrated control and display augmentation for manual remote flight control in the presence of large latency
AU - Zhang, Fubiao
AU - Fricke, Tim
AU - Holzapfel, Florian
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - Large latency in the communication channel presents a huge challenge to effectively remote control the aircraft manually. This paper proposes an approach to alleviate the adverse effect of time delay using control and display augmentation, aiming to improve remote control performance and reduce pilot’s workload. Modest level of automation is necessary for the mission success, the onboard controller admits straightforward influence on the flight path. A reference model based control architecture was employed, the reference model not only acts as the desired dynamics for the onboard controller to track, the same reference model was also used on the ground, giving the pilot undelayed indication of the control command through Head Up Display. Synthetic vision is another feature of the visual system, providing the freedom of feeding aircraft states from nonlinear model based prediction to the pilot. This prediction serves for the purpose including: compensates the downlink delay, bridging data gap due to low update rate, synchronizing ground and on board reference models. Pilot in the loop flight test results showed improvement in the tracking performance with the proposed augmentation.
AB - Large latency in the communication channel presents a huge challenge to effectively remote control the aircraft manually. This paper proposes an approach to alleviate the adverse effect of time delay using control and display augmentation, aiming to improve remote control performance and reduce pilot’s workload. Modest level of automation is necessary for the mission success, the onboard controller admits straightforward influence on the flight path. A reference model based control architecture was employed, the reference model not only acts as the desired dynamics for the onboard controller to track, the same reference model was also used on the ground, giving the pilot undelayed indication of the control command through Head Up Display. Synthetic vision is another feature of the visual system, providing the freedom of feeding aircraft states from nonlinear model based prediction to the pilot. This prediction serves for the purpose including: compensates the downlink delay, bridging data gap due to low update rate, synchronizing ground and on board reference models. Pilot in the loop flight test results showed improvement in the tracking performance with the proposed augmentation.
UR - http://www.scopus.com/inward/record.url?scp=85086054066&partnerID=8YFLogxK
U2 - 10.2514/6.2016-1867
DO - 10.2514/6.2016-1867
M3 - Conference contribution
AN - SCOPUS:85086054066
SN - 9781624103896
T3 - 2016 AIAA Guidance, Navigation, and Control Conference
BT - AIAA Guidance, Navigation, and Control Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Guidance, Navigation, and Control Conference, 2016
Y2 - 4 January 2016 through 8 January 2016
ER -