ETS-LARCASE Laboratory of Active Controls, Aeroservoelasticity and Avionics,Department of Automated Production Engineering 1100 Notre Dame West, Montreal, Que., Canada, H3C1K3 ltgrigorie@yahoo.com;
ETS-LARCASE Laboratory of Active Controls, Aeroservoelasticity and Avionics,Department of Automated Production Engineering 1100 Notre Dame West, Montreal, Que., Canada, H3C1K3 andrei-vladimir.popov.@ens.etsmtl.ca;
ETS-LARCASE Laboratory of Active Controls, Aeroservoelasticity and Avionics,Department of Automated Production Engineering 1100 Notre Dame West, Montreal, Que., Canada, H3C1K3 ruxandra@gpa.etsmtl.ca;
Institute for Aerospace Research, National Research Council,Ottawa, Ontario, K1A 0R6, Canada;
Institute for Aerospace Research, National Research Council,Ottawa, Ontario, K1A 0R6, Canada;
fuzzy logic control; morphing wing; laminar to turbulentrntransition; wind tunnel;
机译:变形机翼应用的新型受控旋转致动系统的设计和风洞实验验证
机译:变形机翼的开-关和比例积分控制器。第2部分:控制验证-数值模拟和实验测试
机译:变形机翼的开-关和比例积分控制器。第2部分:控制验证-数值模拟和实验测试
机译:变形翼的智能控制,第2部分:验证阶段
机译:变形机翼和副翼系统致动系统控制方法的开发与验证=变形机翼和机翼系统致动系统控制方法的开发与验证
机译:变形翼尖驱动系统的基于模糊逻辑的控制:设计数值模拟和风洞实验测试
机译:混合模糊逻辑比例-积分-微分和常规开关控制器,用于使用形状记忆合金变形机翼致动:第2部分,控制器的实现和验证