在线估计飞机状态参数的非线性观测器

Non-linear Observer for on-line Estimating Aircraft States

  • 摘要: 本文介绍了一种同时估计飞行力学状态参数——迎角及侧滑角精度的纵横向运动耦合的具有线加速度反馈的非线性观测器的在线飞行试验研究结果.证实这种观测器不仅结构简单,可以在线实现,而且估计值与实测值令人惊疑的一致,其估计精度已达到了实际飞行导行/控制系统所要求的0.2°范围.此外,还进一步证实,这种观测器具有很好的抗大气紊流干扰及抗工作点(飞行状态)变化的鲁棒性.这些表明,这种观测器可以在线应用于实际飞行导航/控制系统中去.

     

    Abstract: This paper presents a sufficiently accurate,on-line and realizable ronlinear observer,which takes the coupling between longitudinal and lateral motion into accountand is provided with proper feedbacks for all three acceleration components.Such anobserver can be used for estimating simultaneously the angle of attack and ship angle from accurately measured flight test data under either steaoy or nonsteady manoeuver conditions.As we know,the common sensor(wind vane)is not able to measureaccurately both the angle of attack and the side slip angle.In order to make it on-lineapplicable to a flight control/navigation system,the authors employ a simplifiedsecond order observer in this paper.It is proved by on-line estimated results from flight test data that the observerhas not only very good estimation qualities in different flight monceuvers,meeting there quired accuracy of 0.2°in the flight control/navigation system,but also very strongro bustness against stochastic atmospheric turbulence and drastic changes of flight conditions.It indicates that this observer can be applied to actual system.

     

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