Search
Code Directory
 ASP
 ASP.NET
 C/C++
 CFML
 CGI/PERL
 Delphi
 Development
 Flash
 HTML
 Java
 JavaScript
 Pascal
 PHP
 Python
 SQL
 Tools
 Visual Basic & VB.NET
 XML
New Code
Spire.PDF for Java 2.7.8
Database Workbench Pro 5.6.10.0
The C# PDF Library 2020.1.5
CAD-Viewer 3DVBVIEW V4
dotConnect for SQLite 5.15
LuaStudio 9.92
EntityDAC 2.3
Devart ODBC Driver for QuickBooks 2.0
phpEnter 5.1.
Udemy Clone script 2.01
VisualNEO Web 19.11.7
VisualNEO for Windows 19.4.29.0
SentiVeillance SDK Trial 7.3
Devart ODBC Driver for PostgreSQL 3.2
SecureBridge 9.2
Top Code
SecureBridge 8.0
dotConnect for SQLite 5.9
EntityDAC 1.6
Database Workbench Pro 5.6.10.0
ATN Site Builder 3.0
ATN Resume Finder 2.0
PHP Review Script 1.0
ICPennyBid Penny Auction Script 4.0
Invoice Manager by PHPJabbers 3.0
Devart ODBC Driver for PostgreSQL 3.2
The C# PDF Library 1.0
Aglowsoft SQL Query Tools 8.2
Classified Ad Lister 1.0
Solid File System OS edition 5.1
ADO.NET Provider for ExactTarget 1.0
Top Rated
phpEnter 5.1.
Single Leg MLM 1.2.1
Azizi search engine script PHP 4.1.10
Paste phpSoftPro 1.4.1
Extreme Injector 3.7
Deals and Discounts Website Script 1.0.2
ADO.NET Provider for ExactTarget 1.0
Solid File System OS edition 5.1
Classified Ad Lister 1.0
Aglowsoft SQL Query Tools 8.2
Invoice Manager by PHPJabbers 3.0
ICPennyBid Penny Auction Script 4.0
PHP Review Script 1.0
ATN Resume Finder 2.0
ATN Site Builder 3.0
MATLAB simulation of fixed-mass rigid-body 6DOF 1.0
File ID: 79344






MATLAB simulation of fixed-mass rigid-body 6DOF 1.0
Download MATLAB simulation of fixed-mass rigid-body 6DOF 1.0http://www.mathworks.comReport Error Link
License: Freeware
File Size: 10.0 KB
Downloads: 64
User Rating:1 Stars  (1 rating)
Submit Rating:
MATLAB simulation of fixed-mass rigid-body 6DOF 1.0 Description
Description: SIXDOF Calculate aircraft fixed-mass rigid-body six-degrees-of-freedom
equations of motion using MATLAB ODE45 solver.

=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
Inputs:
=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
Forces = 3x1 vector of forces in body coordinates
Moments = 3x1 vectory of moments in body coordinates
Mass = fixed mass of the aircraft
Inertia = 3x3 Inertia Tensor matrix
tarray = time series vector

OPTIONAL INPUTS:
Ipos_i = 3x1 vector of initial position
Ivel_b = 3x1 vector of initial velocity (body)
Irates_b = 3x1 vector of initial body rates
Ieuler = 3x1 vector of initial euler angles

=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
Outputs:
=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
t = simulation time
y(1:3) = body rates
y(4:6) = velocity in body coordinates
y(7:9) = position in body coordinates

License: Freeware

Related: forces, velocity, Time, Simulation, inputs, outputs, inertia, vectory, Vector, Position, fixed, matlab ode, time series vector, aircraft inertia, tensor matrix tarray, vector optional inputs, velocity body irates, Body, 3d 3x3, 3d 3x1

O/S:BSD, Linux, Solaris, Mac OS X

File Size: 10.0 KB

Downloads: 64



More Similar Code

SIXDOFVM Calculate aircraft variable-mass rigid-body six-degrees-of-freedom
equations of motion using MATLAB ODE45 solver.

=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
Inputs:
=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=-=
Forces = 3x1 vector of forces in body coordinates
Moments = 3x1 vectory of moments in body coordinates
dMass = mass rate of change for the aircraft
dInertia = 3x3 Inertia...



findEulerAngs generates Euler angle sets and animates rotations in response to user manipulation of a 3D rigid body (a box).

Use the mouse to change the orientation of the box. A wireframe of the original box position will appear. The...



This is a fully three-dimensional rigid body simulation engine. The bodies are unconstrained. This example demonstrates the simulation of a triple pendulum: three prismatic bars connected by springs bounce and swing freely.



These function implement Lie integrators to perform long time simulation of a rigid body in a static spring-magnetic potential field. This numerical test of symplecticity is detailed in:

Bou-Rabee, N., Ortolan, G., and Saccon, A....



The dynamics of the rotational motion of a rigid body is simulated with this functional library block. This block is intended for simulation (academic) purposes, where the time history of the angular velocity vector is provided.

This...



Rigid body 2-D image co-registration (translation and rotation) is performed using maximization of mutual information.

Function is implemented in c-code and compiled using the Matlab compiler to minimize computation time. Current...



Simulation of Trajectory of Two-body system, sun and earth in this case.



AQUILA is a MATLAB toolbox for the one- or two dimensional simulation of the electronic properties of GaAs/AlGaAs semiconductor nanostructures. The program solves for a user-defined structure the one- or twodimensional Schroedinger- and...



This collection contains M-files intended for design of the Mass/Damper/Spring control system using the newly available functions from Robust Control Toolbox,version 3. Description of the system and version of the files using functions from...



Explain why we use fftshift(fft(fftshift(x))) in Matlab instead of fft(x). An example is given. The example and Matlab codes are partially copied from Daniele Disco d-de?s work in "A guide to the Fast Fourier Transform, 2nd Edition".

User Review for MATLAB simulation of fixed-mass rigid-body 6DOF
- required fields
     

Please enter text on the image