Satellite Trajectory
Tool for visualizing spacecraft trajectory around a planet in various coordinate systems.
编者注: This file was selected as MATLAB Central Pick of the Week
Inputs are the Keplerian orbital elements, planet properties, and ground station coordinates. Tabs include plots of spacecraft trajectory in the following coordinate systems:
Perifocal
Planet-Centered Inertial
Earth-Centered, Earth-Fixed (Planet-Centered Rotational)
East-North-Up
Groundtrack
Horizontal
Includes animation and slider controls for plotting the position of the spacecraft within the time frame defined from the time of periapsis passage, tau, to an arbitrary time, t_1. Four example .ini configurations are included to demonstrate usage.
Units are in SI (km) with options to select degrees or radians (as of version 1.1.0).
引用格式
Huy Nguyen (2026). Satellite Trajectory (https://ww2.mathworks.cn/matlabcentral/fileexchange/85273-satellite-trajectory), MATLAB Central File Exchange. 检索时间: .
致谢
参考作品: INI Config
| 版本 | 已发布 | 发行说明 | Action |
|---|---|---|---|
| 1.2.1.1 | Updated About |
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| 1.2.1 | Units are now in degrees by default
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| 1.2.0.1 | Updated screenshot for version 1.2.0 |
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| 1.2.0 | - Now displays current spacecraft position and time in plots
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| 1.1.1 | Minor fixes. |
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| 1.1.0.1 | Updated screenshot for version 1.1.0 |
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| 1.1.0 | See changelog.txt |
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| 1.0.0 |
