Research on Trim Control of Compound High Speed Helicopter

• 作 者: YU Zhiming KONG Weihong CHEN R
• 机 构: NationalKeyLaboratoryofScienceandTechnologyonRotorcraftAeromechanics
• 出 处: 南京航空航天大学学报:英文版
• 发表日期: 2019年3期
• 关键词: COMPOUND HELICOPTER TRIM CONTROL OPTIMIZATION
• 基金项目: supported by the National Natural Science Foundation of China(No.51505216).

An investigation is conducted on optimizing the control allocation for trimmed flight on the compound helicopter.The compound helicopter features a single main rotor,a vectored thrust ducted propeller(VTDP)and lifting wings.Due to the redundant controls f