table with determining the maximum slope to control an aircraft in bodenfolgeflug

• 1. 无线通信系统中的群确收和/或群否定确收 [P] . 中国专利： CN110546904A . 2019-12-06
• 2. 用于管理无线电链路控制(RLC)不确收模式(UM)中的超帧号(HFN)去同步的装置和方法 [P] . 中国专利： CN104718716B . 2018.09.28
• 3. table with determining the maximum slope to control an aircraft in bodenfolgeflug [P] . 德国专利： DE602005001801D1 . 2007-09-13

  机译： 确定在bodenfolgeflug中控制飞机的最大坡度的表格

• 4. Flight control indicator determining the maximum slope for the flight control of an aircraft by terrain following [P] . 美国专利： US7089090B2 . 2006-08-08

  机译： 飞行控制指示器，通过地形跟踪确定飞机飞行控制的最大坡度

• 5. Flight control indicator determining the maximum slope for the flight control of an aircraft by terrain following [P] . 美国专利： US2005273221A1 . 2005-12-08

  机译： 飞行控制指示器，通过地形跟踪确定飞机飞行控制的最大坡度

• 1. Maximum Power Point Tracking in Variable Speed Wind Turbine Based on Permanent Magnet Synchronous Generator Using Maximum Torque Sliding Mode Control Strategy [J] . Esmaeil Ghaderi, Hossein Tohidi, Behnam Khosrozadeh 电子科技学刊：英文版 . 2017,第004期
• 2. ESTIMATION OF HANKINSON FORMULA, MAXIMUM STRESS THEORY AND TSAI-HILL FAILURE THEORY TO DETERMINE THE STRENGTH OF 3-PLY LAMINATED VENEER LUMBER WITH GRAIN SLOPE [C] . Sei-Chang Oh World conference on timber engineering . 2010
• 3. Adaptive glide slope control for parafoil and payload aircraft [D] . Ward, Michael 2012
• 4. A Multilaboratory Multicountry Study To Determine MIC Quality Control Ranges for Phenotypic Drug Susceptibility Testing of Selected First-Line Antituberculosis Drugs Second-Line Injectables Fluoroquinolones Clofazimine and Linezolid [O] . Koné Kaniga, Daniela M. Cirillo, Sven Hoffner, 2016
• 5. Table 2: Means and standard error (se) of heating rate (c*1,000; c in °C/s) and maximum temperature (asymptote; °C) during heating trials under laboratory conditions by seven taxa of dung beetles (Scarabaeinae) according to sex and two sources of radiation. Figures are adjusted means after controlling for the influence of three covariates in the ANCOVA models of Tables 3 and 4. [O] . -1
• 6. Determining the Maximum Number of Radar Controlled Interceptor Aircraft by a Tactical Air Defense System [R] . Clements, D. W. 1987

• 1. Reservoir controlling differences between consequent faults and antithetic faults in slope area outside of source: A case study of the south-central Wenan slope of Jizhong Depression, Bohai Bay Basin, East China [J] . LIU Junqiao ,CAO Lanzhu ,WANG Haixue . 石油勘探与开发 . 2018,第001期
• 2. Maximum Power Point Tracking in Variable Speed Wind Turbine Based on Permanent Magnet Synchronous Generator Using Maximum Torque Sliding Mode Control Strategy [J] . Esmaeil Ghaderi ,Hossein Tohidi ,Behnam Khosrozadeh . 电子科技学刊 . 2017,第004期
• 3. Influence of Wall Effect on Comprehensive Controllability for Ducted Fan Aircraft [J] . Tianfu Ai ,Changle Xiang ,Bin Xu . 北京理工大学学报：英文版 . 2020,第4期
• 4. Determining the approach speed envelope of carrier aircraft [J] . Geng Jianzhong ,Yao Hailin ,Duan Zhuoyi . 中国工程科学 . 2013,第006期
• 5. 功能性限定在专利授(确)权程序、侵权纠纷程序中的影响 [C] . 马丽丽 . 2016年专利代理学术研讨会 . 2016
• 6. PID控制器参数模糊自整定在智能家电控制中的应用 [A] . 魏新生 . 2005