Description: STK 是卫星仿真工具包,由美国AGI开发的一款在航天工业领域中处于绝对领先地位的商品化分析软件。这里附上的是这个软件的教程。-STK is a satellite simulation tool kit developed by the United States AGI a field in the aerospace industry in the commercialization of the absolute leading position analysis software. Here attached is the software tutorial. Platform: |
Size: 9157632 |
Author:朝霞 |
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Description: This model shows NASA s HL-20 lifting body modeled in Simulink, and Aerospace Blockset. This model simulates approach and landing flight phases using an auto-landing controller. Platform: |
Size: 37888 |
Author:wanghuixia |
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Description: This model simulates a six-degrees-of-freedom variable mass equations of motion with Simulink and Aerospace Blockset. This
model has been color coded to aid in locating Aerospace Blockset blocks. The red blocks are Aerospace Blockset blocks, the orange blocks are subsystems containing additional Aerospace Blockset blocks and the white blocks are Simulink blocks. Platform: |
Size: 19456 |
Author:wanghuixia |
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Description: This demonstration models a flight control for the longitudinal motion of a Grumman Aerospace F-14 Tomcat. First order linear
approximations of the aircraft and actuator behavior are connected to an analog flight control design that uses the pilot s
stick pitch command as the set point for the aircraft s pitch attitude and uses aircraft pitch angle and pitch rate to determine commands. A simplified Dryden wind gust model is incorporated to perturb the system. Platform: |
Size: 11264 |
Author:wanghuixia |
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Description: 自适应滑模控制程序,现在自适应控制在航空航天应用的比较多,将滑模控制和自适应控制结合起来,有其他控制方法无法比拟的优势-Adaptive sliding mode control process, and now Adaptive control in aerospace applications more to sliding mode control and adaptive control combined control method has other advantages beyond compare Platform: |
Size: 1024 |
Author:苏是 |
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Description: 螺旋桨PID控制
In response to constant pressure to design more efficient, faster, smaller, and better systems, engineers are constantly looking for ways to improve existing designs or replace them with better ones. Facing large fuel costs, the aerospace industry in particular has been researching alternative designs to increase fuel efficiency and performance. One such alternative is the development of reconfigurable aircraft wings. These wings would be able to adapt to the current environment increasing lift or reducing drag when appropriate. -PID control of the propeller In response to constant pressure to design more efficient, faster, smaller, and better systems, engineers are constantly looking for ways to improve existing designs or replace them with better ones. Facing large fuel costs, the aerospace industry in particular has been researching alternative designs to increase fuel efficiency and performance. One such alternative is the development of reconfigurable aircraft wings. These wings would be able to adapt to the current environment increasing lift or reducing drag when appropriate. Platform: |
Size: 1024 |
Author:王晨至 |
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Description: 利用模糊卡尔曼滤波器实现航空航天器的遥测遥控,在测控领域具有重要的应用价值。-Fuzzy Kalman filter implementation of aerospace remote sensing and control, measurement and control have important application value. Platform: |
Size: 234496 |
Author:流水 |
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Description: 《MATLAB有限元分析与应用》(德国)(P.l.Kattan)卡坦:采用当今在工程和工程教育方面非常流行的数学软件MATLAB,对有限元分析进行数值实现。书中既包含了MATLAB的简单介绍,又详述了有限元方法的系统性处理策略,并提供了大量取自机械工程、土木工程、航空航天工程或材料科学的示例和习题,非常适合相关专业的学生和研究人员使用。《MATLAB有限元分析与应用》特别强调对MATLAB的交互应用,书中的每个示例都以交互的方式求解,有利于读者切实提高有限元的分析和应用能力。以上代码为本书源代码。
-"MATLAB finite element analysis and application" (Germany) (PlKattan) Catan: using today s engineering and engineering education in the popular mathematical software MATLAB, the finite element analysis numerical implementation. The book not only contains a brief introduction to MATLAB, and the finite element method described systematic processing strategy, and provides a large number from the mechanical engineering, civil engineering, aerospace engineering or materials science examples and exercises, ideal for relevant professional Students and researchers. "MATLAB finite element analysis and application of"special emphasis on the MATLAB interactive applications, each of the examples in the book the way to solve the interaction is conducive to the reader effectively improve the finite element analysis and application. Source code for the book above.
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Size: 258048 |
Author:刘雨霰 |
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Description: matlab的轨道力学子程序,适用于搞航天航空的专业人士学习和使用。-matlab subroutine of orbital mechanics, for aerospace professionals to engage in learning and use. Platform: |
Size: 476160 |
Author:天马 |
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Description: MIT--航空航天工程中的计算方法_模拟飞机的动力学
MIT公开课程--航空航天工程中的计算方法
这门课程适用于在航空和航天工程中出现的计算方法的入门学习。其应用是从航空宇宙结构,空气动力学,动力学和控制,和航空宇宙系统选出的。其技术包括:常微分方程系统的数值积分;偏微分方程式的有限差分,有限体积, 和有限元的离散化;数值线性代数;本征值问题和带有约束的最优化。-MIT- Aerospace Engineering in the calculation of simulated aircraft dynamics _ MIT Open Course- Aerospace engineering calculation methods for this course in aviation and aerospace engineering calculations appear in an introduction. The application is from aerospace structures, aerodynamics, dynamics and control, and aerospace systems selected. The technologies include: numerical integration of ordinary differential equations systems partial differential equations of finite difference, finite volume, and finite element discretization numerical linear algebra eigenvalue problems with constraints and optimization. Platform: |
Size: 300032 |
Author:skp |
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Description: MIT--航空航天工程中的计算方法_模拟可变面积管道中的可压缩无粘滞流体
MIT公开课程--航空航天工程中的计算方法
这门课程适用于在航空和航天工程中出现的计算方法的入门学习。其应用是从航空宇宙结构,空气动力学,动力学和控制,和航空宇宙系统选出的。其技术包括:常微分方程系统的数值积分;偏微分方程式的有限差分,有限体积, 和有限元的离散化;数值线性代数;本征值问题和带有约束的最优化。
-MIT- Aerospace engineering calculations _ simulation of compressible variable-area duct without viscous fluid MIT Open Course- Aerospace engineering calculation methods for this course in aviation and aerospace engineering calculations appear method of getting started. The application is from aerospace structures, aerodynamics, dynamics and control, and aerospace systems selected. The technologies include: numerical integration of ordinary differential equations systems partial differential equations of finite difference, finite volume, and finite element discretization numerical linear algebra eigenvalue problems with constraints and optimization. Platform: |
Size: 422912 |
Author:skp |
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Description: MIT--航空航天工程中的计算方法_有限元方法实例——涡轮叶片传热
MIT公开课程--航空航天工程中的计算方法
这门课程适用于在航空和航天工程中出现的计算方法的入门学习。其应用是从航空宇宙结构,空气动力学,动力学和控制,和航空宇宙系统选出的。其技术包括:常微分方程系统的数值积分;偏微分方程式的有限差分,有限体积, 和有限元的离散化;数值线性代数;本征值问题和带有约束的最优化。
-MIT- Aerospace Engineering in the finite element method calculation _ instance- turbine blade heat transfer MIT Open Course- Aerospace engineering calculation methods for this course in aviation and aerospace engineering in the calculation of the entry appears to learn. The application is from aerospace structures, aerodynamics, dynamics and control, and aerospace systems selected. The technologies include: numerical integration of ordinary differential equations systems partial differential equations of finite difference, finite volume, and finite element discretization numerical linear algebra eigenvalue problems with constraints and optimization. Platform: |
Size: 268288 |
Author:skp |
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Description: MIT--航空航天工程中的计算方法_概率论方法实例——涡轮叶片中的热传导问题
MIT公开课程--航空航天工程中的计算方法
这门课程适用于在航空和航天工程中出现的计算方法的入门学习。其应用是从航空宇宙结构,空气动力学,动力学和控制,和航空宇宙系统选出的。其技术包括:常微分方程系统的数值积分;偏微分方程式的有限差分,有限体积, 和有限元的离散化;数值线性代数;本征值问题和带有约束的最优化。-MIT- Aerospace engineering calculation methods of probability theory _ instance- turbine blade heat conduction problem in the MIT Open Course- Aerospace engineering calculation methods for this course in aviation and aerospace engineering calculation methods appear of getting started. The application is from aerospace structures, aerodynamics, dynamics and control, and aerospace systems selected. The technologies include: numerical integration of ordinary differential equations systems partial differential equations of finite difference, finite volume, and finite element discretization numerical linear algebra eigenvalue problems with constraints and optimization. Platform: |
Size: 331776 |
Author:skp |
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Description: 航天方向轨道相关函数库,包含许多小程序,方便调用,通用性强(function lib of aerospace aspects, including many small but useful functions. can be used easily and very readable.) Platform: |
Size: 498688 |
Author:hisjn2017
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