Description: 旅行问题,是我的第一个C作业,是关于飞机积分的计算问题,程序还是比较简单的.
-travel, I was the first one C operations, the aircraft is on the integral calculation, procedure is relatively simple. Platform: |
Size: 829 |
Author:jack |
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Description: 在某初教机的线性模型基础上，建立了飞机的纵向和横向传递函数，分析了模型参数的不确定性，通过使用MATLAB中的NCD模块对飞行控制系统及PID控制器等参数进行优化，设计出了飞机的自动驾驶仪高度保持和航向保持模式。这种方法既避免了复杂的计算和编程，又使系统具有较好的稳定，陛、动态性能和鲁棒性，克服了飞机模型参数随着高度和速度的变化（即模型参数存在不确定性）而需要按照多个不同高度和速度的飞行区域设计一系列控制器的缺点-early in a plane of the linear model, based on the aircraft's vertical and horizontal transfer function, Analysis of the model parameters of uncertainty, MATLAB through the use of the NCD Blocks flight control system and PID controller parameters for optimization, design of the aircraft's automatic pilot systems, and maintain a high degree course-keeping mode. This method not only avoids the complex calculation and programming, the system has good stability, Her Majesty, dynamic performance and robustness. overcome the aircraft model parameters with the height and speed of change (that model parameters uncertainty exists) and the need to not more than with the height and speed of regional flight controller design a series of shortcomings Platform: |
Size: 278096 |
Author:jake |
Hits:
Description: 旅行问题,是我的第一个C作业,是关于飞机积分的计算问题,程序还是比较简单的.
-travel, I was the first one C operations, the aircraft is on the integral calculation, procedure is relatively simple. Platform: |
Size: 1024 |
Author:jack |
Hits:
Description: 在某初教机的线性模型基础上，建立了飞机的纵向和横向传递函数，分析了模型参数的不确定性，通过使用MATLAB中的NCD模块对飞行控制系统及PID控制器等参数进行优化，设计出了飞机的自动驾驶仪高度保持和航向保持模式。这种方法既避免了复杂的计算和编程，又使系统具有较好的稳定，陛、动态性能和鲁棒性，克服了飞机模型参数随着高度和速度的变化（即模型参数存在不确定性）而需要按照多个不同高度和速度的飞行区域设计一系列控制器的缺点-early in a plane of the linear model, based on the aircraft's vertical and horizontal transfer function, Analysis of the model parameters of uncertainty, MATLAB through the use of the NCD Blocks flight control system and PID controller parameters for optimization, design of the aircraft's automatic pilot systems, and maintain a high degree course-keeping mode. This method not only avoids the complex calculation and programming, the system has good stability, Her Majesty, dynamic performance and robustness. overcome the aircraft model parameters with the height and speed of change (that model parameters uncertainty exists) and the need to not more than with the height and speed of regional flight controller design a series of shortcomings Platform: |
Size: 277504 |
Author:jake |
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Description: 由于飞机设计是一个需要多次反复迭代的重复过程，需要进行大量的计算，因此我们自己编写了一些MATLAB程序。-As the aircraft design is a repeated duplication of iterative process, requiring a large number of calculation, so we have written a number of MATLAB procedures. Platform: |
Size: 29696 |
Author:白锋 |
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Description: 该程序是按照矩阵位移法的后处理法的基本原理和分析过程，并借助 Visual Basic 所设计的，适用于平面珩架在节点静力荷载作用下的内力与位移计算问题。
主要功能包括：节点位移，杆件轴力的计算；珩架节点位移的动态演示； work plane上的增添、修改、查询等可视化操作；输入文档与输出文档
-That the procedure was in accordance with the matrix displacement method of post-processing method and analysis of the basic principles of process and using Visual Basic is designed for aircraft in the node plane Heng static load calculation of internal force and displacement. The main features include: node displacement, axial force bar calculation Heng plane displacement dynamic presentation node work plane on to add, modify, query, such as visualization to operate input documents and output documents Platform: |
Size: 1033216 |
Author:luozhongquan |
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Description: ASCII:运行后会显示一个完整的Ascii码表。
医院体检录入:运行后有菜单选择录入新数据，还是查看现有数据，录入时有对输入数据的校验，保证录入的正确。
计算大数阶乘:采用非常优秀的递归算法,轻松算出大数的阶乘.
飞机大战:控制一个飞机打屏幕上的飞机，涉及到各种键控技术，同时也是一种分时处理的技术。
模拟电子琴:通过按数字键发出不同高低的音调。一个控制发声的小程序。
模拟霓虹灯:一个可以模拟霓虹灯效果的小程序-ASCII: running will display a complete Ascii code table. Hospital medical entry: menu to select run after the entry of new data, or view the existing data entry when the validation of input data, and ensure the correct entry. Calculation of factorial of large numbers: The recursive algorithm is very good, easy to calculate the factorial of large numbers. World War II aircraft: the control of an aircraft hit the screen on the plane, involving a variety of keying technology, but also deal with a time-sharing technology. Simulated electronic organ: by pressing the number keys of different high and low tones. A small voice control procedures. Simulation of neon: neon lights to simulate the effect of a small program Platform: |
Size: 74752 |
Author:高世鹏 |
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Description: 飞机起飞性能计算，确定飞机的起飞性能，包括滑跑距离、起飞距离、起飞时间、离地速度，气动修正考虑了收放起落架、襟翼的影响，但未考虑地面效应.-Aircraft take-off performance calculations to determine the aircraft s takeoff performance, including the roll distance, takeoff distance, takeoff time, off speed, the amendment takes into account pneumatic retractable landing gear, flaps impact, but did not consider ground effect. Platform: |
Size: 2048 |
Author:李朋 |
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Description: 飞机机动性能计算，确定飞机的正常盘旋性能，包括过载、盘旋半径和盘旋周期-Calculation of mobility aircraft, the aircraft circled the normal performance, including overload, circled and circled radius cycle Platform: |
Size: 3072 |
Author:李朋 |
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Description: A组
用汇编语言实现：在屏幕上显示：
SIN（X）+345*X/67
X=？
REXUILT=
等待输入一个任意的十进制数X（假设每个数不超过三位），计算上述表达式的结果，将该结果显示出来：对于XIN（X）的计算结果要求采用子程序编写，主程序用于输入X和显示结果。
B组：
汇编程序写一个能与PC当前运行的程序进行分时操作的程序，程序的功能是演奏“五星红旗迎风飘扬”。并设置有热键，可随时终止或恢复演奏。
C组：
用汇编程序编程编写一个动画程序：有一架飞机在显示屏幕的上方，从左至右，忽高忽地，周而复始的飞行，屏幕下方设有一门高射炮，该炮可人工控制左右移动，人工控制空格键发射炮弹，炮弹命中飞机后，声光大作。（要求使用图形显示方式）
-A group
Using assembly language to achieve: on the screen:
SIN (X)+345* X/67
X =?
REXUILT =
Waiting for input an arbitrary decimal number X (the assumption that the number of not more than three each), calculated the results of the above expression, the results are displayed: For XIN (X) requires the calculation of the results of the preparation subroutine, main program for Enter the X and the result will be displayed.
B:
Assembler to write a PC currently running with the process time-sharing operating procedures, procedures for the function is to play "five-star red flag fluttering in the wind." And set up hotkeys, may terminate or resume play.
C:
Used to prepare a compilation of animated programming process: a plane in the display screen above, from left to right, then high忽地, the flight cycle, the bottom of the screen with an anti-aircraft gun, the gun can be moved about manual control, manual control and air Grid button fired artillery shells that hit the airc Platform: |
Size: 38912 |
Author:王林 |
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Description: 题目所给飞机机翼受的是平均载荷，所以要计算每一站点上的剪力，弯矩和扭矩，就要先算出其所在平面的面积和其合力作用线到某一座标轴的距离，及集中载荷作用线到中心线的距离。带载荷等于面积乘以平均载荷，某一站点剪力等于此站点之前所有带载荷之和。弯矩等于剪力乘以合力作用线到其对应坐标轴的距离。扭矩等于剪力乘以集中载荷作用线到中心线的距离。所得结果与笔算结果基本吻合。程序具有一定的通用性。-Subject to the aircraft wing by the average load is, so each site to calculate shear, moment and torque, we must first calculate its area in the plane and its force action line to the distance of a coordinate axis , and concentrated load line to the centerline distance. With a load equal to area multiplied by the average load, a shear force equal to this site before the site with loads of and all. Multiplied by the effect of shear force bending moment is equal to the corresponding axis line to the distance. Torque multiplied by the concentrated load is equal to the shear line to the centerline distance. The results results are consistent with written calculation. Program has some versatility. Platform: |
Size: 9216 |
Author:天云 |
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Description: 飞机强度计算中的有限元与CAD_CAM一体化的讲解说明的课件，很有用的，大家下载看看吧-Aircraft strength calculation of the integration of finite element and CAD_CAM explained that the courseware, very useful, we look at it download Platform: |
Size: 133120 |
Author:yeong |
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Description: 飞机大角度攻击的模型仿真程序，描述了在大角度攻击时的姿态控制参数的计算。-Model for large angle of attack aircraft simulation program, described the attack in the large angle attitude control parameter calculation. Platform: |
Size: 2048 |
Author:wangyu |
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Description: 该程序包括了飞行器轨迹计算、陀螺和加速度计的采样输入、以及由四元素解算出的飞行器姿态、位置、速度-The program includes the aircraft trajectory calculation, the sampling gyro and accelerometer input, and the solution calculated by the four elements of aircraft attitude, position, velocity Platform: |
Size: 2048 |
Author:苏钰 |
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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: 对飞机起飞重量进行迭代估算，用户通过GUI界面对任何默认参数可随意修改，适用性较强-Iterating the aircraft takeoff weight estimate, the user through the GUI interface for any default parameters can be freely modified, strong applicability Platform: |
Size: 10240 |
Author:whb |
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Search - aircraft calculation