Identifying the cruising dynamics of a medium scale UAV I: Longitudinal dynamics

机译：识别中等规模UAV I的巡航动态：纵向动态

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Pitch and airspeed responses of a medium scale UAV were identified using the prediction error method. Data collection was conducted with an active closed loop autopilot control system. A naive SISO open loop transfer function was estimated using the parametric direct approach. Since its predictability was not significant, better estimators were developed using MISO parametric direct, and SISO parametric indirect method. The model validations were done to quantify their predictability.

机译：使用预测误差方法识别中等规模UAV的间距和空速响应。使用主动闭环自动驾驶仪控制系统进行数据收集。使用参数直接方法估计天真的Siso开环传递函数。由于其可预测性并不重要，因此使用MISO参数直接开发了更好的估计器，以及SISO参数间接方法。模型验证已完成以量化其可预测性。

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《Moratuwa Engineering Research Conference》|2015年||共6页
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Gamage C.I.; Samarasekera S.C.; Tennakoon A.; Lalantha R.; Munasinghe R.;
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正文语种
中图分类输配电工程、电力网及电力系统;
关键词
MUAV; System identification; closed loop identification; indirect method;

机译：muav;系统识别;闭环识别;间接方法;

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Identifying the cruising dynamics of a medium scale UAV I: Longitudinal dynamics

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