Satellite Trajectory
Tool for visualizing spacecraft trajectory around a planet in various coordinate systems.
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編集メモ: 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
Huy Nguyen (2026). Satellite Trajectory (https://jp.mathworks.com/matlabcentral/fileexchange/85273-satellite-trajectory), MATLAB Central File Exchange. に取得済み.
謝辞
ヒントを得たファイル: INI Config
| バージョン | 公開済み | リリース ノート | 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 |
