01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
MISSION-PROFILE-BASED HYBRID POWER SYSTEM DESIGN AND OPTIMIZATION FOR VTOL AIRCRAFT IN REGIONAL AIR MOBILITY
G. Shen¹, X. Zhang¹, W. Hao¹, Z. Wang¹; ¹Northwestern Polytechnical University, China
This study proposes a mission-profile-based hybrid power system design method for regional AAM VTOL aircraft and applies it to a 500 km-range VTOL aircraft power system. An improved differential evolution algorithm is also introduced for power system optimization.
DOI: 10.71945/icas2026_0696