Piloted Simulation-Based Assessment of Simplified Vehicle Operations for Urban Air Mobility

被引:3
作者
Chakraborty, Imon [1 ]
Comer, Anthony [1 ]
Bhandari, Rajan [1 ]
Putra, Stefanus Harris [1 ]
Mishra, Aashutosh Aman [1 ]
Schaller, Ross [2 ]
Sizoo, David [2 ]
Mcguire, Robert [3 ]
机构
[1] Auburn Univ, Dept Aerosp Engn, Auburn, AL 36849 USA
[2] FAA Compliance & Airworthiness Div, Kansas City, MO 64106 USA
[3] FAA William J Hughes Tech Ctr, FAA Flight Controls & Mech Syst Program, Atlantic City, NJ 08405 USA
来源
JOURNAL OF AEROSPACE INFORMATION SYSTEMS | 2024年 / 21卷 / 05期
关键词
Urban Air Mobility; Flight Control Surfaces; Aircraft Flight Control System; Flight Instructor; Aircraft Components and Structure; Fixed Wing Aircraft; Total Energy Control System; Rotorcrafts; Vertical Takeoff and Landing; Handling Qualities; REAL-TIME; ETHERNET;
D O I
10.2514/1.I011249
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This work investigates the simplified vehicle operations paradigm, which seeks significant reductions in pilot workload and training requirements through the holistic design of flight control laws, control inceptors, and cockpit displays in the context of vertical takeoff and landing urban air mobility aircraft using piloted flight simulations. Two inceptor layouts, one similar to conventional fixed-wing aircraft and the other similar to conventional rotorcraft, differing in inceptor-to-command mappings, were incorporated into two research flight simulators. A lift-plus-cruise aircraft simulation model, a total energy control system-based fly-by-wire flight control architecture, and identical cockpit displays were used for both setups. Twenty-one participants, divided into three groups based on their prior piloting experience, were used to study pilot performance using representative handling qualities task elements. The piloted simulation data revealed that participants in each group were able to successfully perform the simulation tasks and allowed handling quality ratings to be calculated. They also highlighted instances of control coupling between inceptor axes in each setup for different tasks and the relative ease or difficulty of performing each task with the two inceptor designs.
引用
收藏
页码:392 / 421
页数:30
相关论文
共 61 条
[1]  
[Anonymous], 2018, Lilium
[2]  
[Anonymous], 2018, Volocopter
[3]  
[Anonymous], 2019, A Rational Construct for Simplified Vehicle Operations (SVO)
[4]  
[Anonymous], 2020, Vertiport for electric vertical takeoff and landing aircraft
[5]  
[Anonymous], 2020, URBAN AIR MOBILITY U
[6]  
[Anonymous], 2018, eVTOL-The Future of On-Demand Air Transport
[7]  
[Anonymous], 2018, "Modular Generalized Framework for Assessing Aircraft Aero-Propulsive, Stability, and Control Characteristics
[8]  
[Anonymous], 2019, Pixelwix/Pixelwarp Evo Visual Aid Software
[9]  
[Anonymous], 2000, ADS- 33E-PRF
[10]  
Beringer D., 2002, DOTFAAAM027 CIV AER