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随着直升机的飞行状态的不同,直升机的俯仰角θ和侧倾角γ_s及偏航角α_s也相应改变,最终保证直升机以平衡的、稳定的姿态完成飞行任务。这里着重阐述的是直升机的侧倾角产生原因;直升机各参数对侧倾角大小的影响;侧倾角对飞行姿态及性能的影响及其利用。
As the helicopter’s flight status changes, the helicopter pitch angle θ and roll angle γ_s and yaw angle α_s also change accordingly, and ultimately ensure the helicopter to complete the mission in a balanced and stable attitude. Here are the reasons for the helicopter roll angle; helicopter parameters affect the roll angle size; roll angle on the flight attitude and performance and its use.