«« « 12 » »»
 336 336

### MATLAB Simulation of variable-mass rigid-body 6DOF 1.0

Forces = 3x1 vector of forces in body coordinates

### Airfoil Analyzer 1.0

- Airfoils can be quickly plotted at just selection.

### generate_great_circle_path 1.0

· MATLAB Release: R14SP2

### Trajectory and Attitude Plot 2.0

This function plot in the same figure the center trajectory and attitude of an aircraft. See the figure to understand better.
The version 2.0, extend the functionality of version 1. In this version there are much more body models [for ...

### Understanding the Euler Angles 1.0

Description in short: : An Educating tool.

### Helicopter Rotor motion simulator 1.0

Extensive GUI has been developed with many options and visual aids for better understanding.
Usage PDF file is included with the deatails of how to use and few additional informations about helicoper basics.

### conticap.m 1.0

· MATLAB Release: R14SP1

### Flutter Analysis Model 1.0

This model demonstrates how to implement a coupled structural-aerodynamic problem.

### Earth Albedo Toolbox 1.0

· MATLAB Release: R14SP3

### 2-D Nozzle Design 1.0

a) Solve for the nozzle exit area that produces the max amount of thrust.

### Panel Method Based 2-D Potential Flow Simulator 1.0

- Compute and plot the Velocity Vector Plot of the flow past the selected body

### FDC 1.3.3

· MATLAB Release: R10

### Orbital Mechanics Library 1.0

· MATLAB Release: R13

### MATLAB simulation of fixed-mass rigid-body 6DOF 1.0

Forces = 3x1 vector of forces in body coordinates

### Building Virtual Worlds 1.0

We specifically discuss three demos.

### DCM from Euler angles 1.0

Allowed rotations sequences:

### aero2vr 1.0

· MATLAB Release: R11.1

### Fly a Plane 1.0

Altitude Max 10,000 ft

### Satellite Tracker 1.0

· MATLAB Release: R14

### Airlib 1.0

· MATLAB Release: R11

### Joukowski Airfoil Transformation 1.0

Script that plots streamlines around a circle and around the correspondig Joukowski airfoil. It's obviously calculated as a potential flow and show an approximation to the Kutta-Joukowski Lift.

### Accelerating aircraft design 1.0

- Unzip the files into a new directory

### 6DOF Variable Mass Missile Airframe 1.0

An example of how to simulate variable mass equations of motion with Simulink and Aerospace Blockset (R13 Service Pack 1). The medium blue blocks are Aerospace Blockset blocks and the light blue blocks are subsystems containing additional ...