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热约束下近空间飞行器预设性能抗噪控制
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作者 马悦萌 刘明 +3 位作者 杨丁 杨明 张敏刚 葛亚杰 《航空学报》 EI CAS CSCD 北大核心 2023年第S02期28-40,共13页
近空间高速飞行器再入过程中,巨大的飞行速度将使其面对复杂气动、高温及噪声等严酷的载荷环境。为缓解高速飞行器的热防护结构设计压力,确保再入过程中飞行器的结构与材料安全,从弹道与控制系统设计角度出发,给出近空间高速再入飞行器... 近空间高速飞行器再入过程中,巨大的飞行速度将使其面对复杂气动、高温及噪声等严酷的载荷环境。为缓解高速飞行器的热防护结构设计压力,确保再入过程中飞行器的结构与材料安全,从弹道与控制系统设计角度出发,给出近空间高速再入飞行器攻角约束下的高性能自适应非线性预设性能控制方案,对飞行器进行主动的力热载荷安全管理。首先根据飞行器大面积热流工程模型解算全弹道飞行的攻角约束,结合指数型预设性能函数基于状态受限控制理论对攻角的动态响应过程进行设计,并使用新型前馈Sigmoid非线性跟踪微分器来处理反演控制中的微分爆炸问题;之后引入基于级联的新型扩张状态观测器以抑制传统高增益观测器的峰值现象,通过非线性增益调节机制提高其抗噪能力;并对上述控制系统进行了Lyapunov稳定性证明,从理论上确保了飞行器再入过程中热防护结构强度的安全性。最后给出了本文控制方案与鲁棒-自抗扰控制系统的仿真对比结果。结果表明,本文的控制方案能够确保攻角在预设的性能边界内满足飞行器的力热载荷约束,且在工程噪声环境下具有更稳妥的鲁棒安全保障与更优的指令跟踪性能。 展开更多
关键词 高速飞行器 状态约束 执行机构饱和 预设性能控制 状态估计 抗噪控制
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Active Control of Fan Noise 被引量:2
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作者 Nobuhiko YAMASAKI Hirotoshi TAJIMA 《Journal of Thermal Science》 SCIE EI CAS CSCD 2008年第2期163-169,共7页
In the wake-rotor interaction fan noise, a number of the interacting modes at the blade passing frequency (BPF) and its harmonics are generated which are prescribed by the number of stator and rotor blades etc. In t... In the wake-rotor interaction fan noise, a number of the interacting modes at the blade passing frequency (BPF) and its harmonics are generated which are prescribed by the number of stator and rotor blades etc. In the present study, the dominant mode is tried to be suppressed by the secondary sound from the loudspeaker actuators. One of the novel features of the present system is the adoption of the control board with the Field Programmable Gate Array (FP(3A) hardware and the LabVIEW software to synchronize the circumferentially installed loudspeaker actuators with the relative location of rotational blades under arbitrary fan rotational speeds. The experiments were conducted under the conditions of three rotational speeds of 2004, 3150, and 4002 [rpm]. The reduction in the sound pressure level (SPL) was observed for all three rotational speeds. The sound pressure level at the BPF was reduced approximately 13 [dB] for 2004 [rpm] case, but not so large reduction was attained for other cases probably due to the inefficiency of the loudspeaker actuators at high frequencies 展开更多
关键词 Stator-Rotor Interaction Anti Noise Control (ANC) Cut-on Control
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