# Missile-Target-Engagement-Model

**Repository Path**: cc715/Missile-Target-Engagement-Model

## Basic Information

- **Project Name**: Missile-Target-Engagement-Model
- **Description**: A small test study on guidance of missiles using proportional navigation
- **Primary Language**: Unknown
- **License**: MIT
- **Default Branch**: main
- **Homepage**: None
- **GVP Project**: No

## Statistics

- **Stars**: 0
- **Forks**: 0
- **Created**: 2026-02-05
- **Last Updated**: 2026-02-06

## Categories & Tags

**Categories**: Uncategorized

**Tags**: None

## README

# Missile-Target-Engagement-Model
A small test study on guidance of missiles using proportional navigation
The proportional navigation guidance law issues acceleration commands, perpendicular to the instantaneous missile-target line of sight, which are  proportional to the line-of-sight rate and closing velocity

More details at https://asresearches.wordpress.com/2016/07/01/missile/