| 摘要 |
The angular stabilization fail-safe system for a pilotless aircraft comprises a preset device, the output being connected with the first input of the first adder unit, the output being connected with a regulator, the output being connected with the first of the second adder unit, the output being connected with a servo drive, the output being connected with a pilotless aircraft. The pitching angle and angular velocity data is supplied for pitching angle and angular velocity sensor. There is an integrator, the input being connected with the first angular velocity sensor output and the output is connected with the first input of the first electronic switch. |
