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Attitude control of stratospheric airship with ballonets and elevator

机译:平流层飞艇的高空飞行器姿态控制

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摘要

Air ballonets and elevator are adopted as the main actuators of stratospheric airship in pitch attitude control, actuator dynamics of ballonets and elevator in pitch control are established including the energy consumption models. The varied-weight pseudo inverse method (VWPI) was introduced in control allocation between the ballonets and the elevator in pitch control under different airspeed. The varied weights can be determined by optimal calculation based on the real energy consumption of ballonets and elevator with different airspeed. Optimal control allocation based on pseudo inverse with varied-weights was achieved in pitch control.
机译:在俯仰姿态控制中,采用平流层飞艇的主要致动器为气球和升降舵,在俯仰控制中,建立了芭蕾舞和升降舵的致动器动力学模型,包括能耗模型。在不同空速下的俯仰控制中,在芭蕾舞和电梯之间的控制分配中引入了变权伪逆方法(VWPI)。可以通过基于不同空速的芭蕾舞和电梯的实际能耗,通过最佳计算来确定变化的权重。在变桨控制中实现了基于具有可变权重的伪逆的最优控制分配。

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