TY - GEN
T1 - Dual Pilot Operation Concept for a Tandem Cockpit Fly-By-Wire Trainer Aircraft
AU - Wechner [email protected], Maximilian
AU - Dollinger, Daniel
AU - Holzapfel, Florian
N1 - Publisher Copyright:
© 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2024
Y1 - 2024
N2 - This paper presents a revised concept for dual pilot operations in trainer aircraft with a tandem cockpit configuration. In contrast to existing concepts, like the tandem version of the F-16D, both pilots shall have an equivalent level of authority, and state transients following mode switches shall be avoided. The pilot command source selection and switching concept, which also includes a robust backup control law with virtual trim functionalities, is complemented by a Human-Machine-Interface (HMI) concept. It consists of the related control input items and the pilot feedback items that ensure situational awareness. A safety analysis is performed in the form of a fault tree analysis to verify that no single failure can lead to a loss of control of the aircraft. The overall concept is validated through mission task elements (MTEs) conducted in a prototype simulator. Preliminary handling quality (HQ) evaluations that are also conducted based on the MTE method resulted in an assigned HQ rating of level 2.
AB - This paper presents a revised concept for dual pilot operations in trainer aircraft with a tandem cockpit configuration. In contrast to existing concepts, like the tandem version of the F-16D, both pilots shall have an equivalent level of authority, and state transients following mode switches shall be avoided. The pilot command source selection and switching concept, which also includes a robust backup control law with virtual trim functionalities, is complemented by a Human-Machine-Interface (HMI) concept. It consists of the related control input items and the pilot feedback items that ensure situational awareness. A safety analysis is performed in the form of a fault tree analysis to verify that no single failure can lead to a loss of control of the aircraft. The overall concept is validated through mission task elements (MTEs) conducted in a prototype simulator. Preliminary handling quality (HQ) evaluations that are also conducted based on the MTE method resulted in an assigned HQ rating of level 2.
UR - http://www.scopus.com/inward/record.url?scp=85203677240&partnerID=8YFLogxK
U2 - 10.2514/6.2024-4583
DO - 10.2514/6.2024-4583
M3 - Conference contribution
AN - SCOPUS:85203677240
SN - 9781624107160
T3 - AIAA Aviation Forum and ASCEND, 2024
BT - AIAA Aviation Forum and ASCEND, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Aviation Forum and ASCEND, 2024
Y2 - 29 July 2024 through 2 August 2024
ER -