indulge 发表于 2025-3-21 20:01:08
书目名称Advanced Techniques for Clearance of Flight Control Laws影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0146271<br><br> <br><br>书目名称Advanced Techniques for Clearance of Flight Control Laws影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0146271<br><br> <br><br>书目名称Advanced Techniques for Clearance of Flight Control Laws网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0146271<br><br> <br><br>书目名称Advanced Techniques for Clearance of Flight Control Laws网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0146271<br><br> <br><br>书目名称Advanced Techniques for Clearance of Flight Control Laws被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0146271<br><br> <br><br>书目名称Advanced Techniques for Clearance of Flight Control Laws被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0146271<br><br> <br><br>书目名称Advanced Techniques for Clearance of Flight Control Laws年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0146271<br><br> <br><br>书目名称Advanced Techniques for Clearance of Flight Control Laws年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0146271<br><br> <br><br>书目名称Advanced Techniques for Clearance of Flight Control Laws读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0146271<br><br> <br><br>书目名称Advanced Techniques for Clearance of Flight Control Laws读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0146271<br><br> <br><br>JOG 发表于 2025-3-21 21:24:50
978-3-540-44054-3Springer-Verlag Berlin Heidelberg 2002圆木可阻碍 发表于 2025-3-22 03:17:16
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Biomechanics in Medicine and BiologyTechniques used currently in the aeronautical industry are applied to solve several flight control law clearance tasks. The obtained results for the clearance of the HIRM+RIDE control configuration are intended to serve as basis for comparisons with several more advanced approaches presented in this book.凶兆 发表于 2025-3-22 09:01:10
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Lecture Notes in Control and Information Scienceshttp://image.papertrans.cn/a/image/146271.jpg独白 发表于 2025-3-22 17:27:28
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Barry J. Doyle,Timothy M. McGloughlinght control law clearance problems, . (LFT) based uncertainty models must first be generated to capture the effect of uncertain aircraft parameters on the closed-loop system dynamics. The clearance criteria which are most easily addressed with .-analysis are those which are defined in the frequency跳动 发表于 2025-3-23 06:06:06
Peter A. Huijing,Michael P. Slawnych parameters. These methods basically check the robust stability property of a dynamic system by looking at the characteristic polynomial coefficients. A comparison of the most important Kharitonov type approaches proposed in literature and their applicability to the flight control law clearance prob