A method is presented for unmanned helicopterflightdynamics model identification.
研究了一种无人直升机飞行力学模型辨识方法。
2
In this paper, the rotor power transfer coefficient is determined from the point of helicopterflightdynamics.
文章详细地介绍了从飞行力学的角度来确定直升机平直飞行时的旋翼功率传递系数。
3
Inverse problem of helicopterflightdynamics, to solve control laws from given motion, is important to the study for the maneuvering flight and the design for the advanced flight control system.