【摘要】 在基本飞机构型的条件下,给出机翼载荷控制的目的、方法和效能计算,研究了机动载荷控制系统的设计。通过对某型大展弦比飞机的设计和仿真,表明了控制系统对机翼载荷控制的有效性。更多还原

【Abstract】 Under basic aircraft configuration,the goal,control method and efficient computing of wing load control were presented.The design method of a maneuver load control system was researched.And it shows that the control system is efficient for wing load control through the design and simulation for the certain high-aspect-ratio composite aircraft.更多还原