A MATLAB Script for Optimal Single Impulse De-orbit - SNOPT

バージョン 1.3.0.0 (7.76 MB) 作成者: David Eagle
optimal impulsive maneuver required to de-orbit a spacecraft in a circular or elliptical Earth orbit
0.0
(0)
ダウンロード: 959
更新 2020/4/18

ライセンスの表示

This document describes a MATLAB script named deorbit_snopt that can be used to compute the optimal impulsive maneuver required to de-orbit a spacecraft in a circular or elliptical Earth orbit. The user provides the classical orbital elements of the initial orbit along with geodetic altitude and relative flight path angle targets at the entry interface (EI).

引用

David Eagle (2024). A MATLAB Script for Optimal Single Impulse De-orbit - SNOPT (https://www.mathworks.com/matlabcentral/fileexchange/38907-a-matlab-script-for-optimal-single-impulse-de-orbit-snopt), MATLAB Central File Exchange. 取得済み .

MATLAB リリースの互換性
作成: R2011b
すべてのリリースと互換性あり
プラットフォームの互換性
Windows macOS Linux

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!

バージョン 公開済み リリース ノート
1.3.0.0

Updated PDF document and code cleanup.
1.2.0.0

Added version of main script (deorbit_snopt_64bit) that uses the March 17, 2014 version of SNOPT.
1.1.0.0

Added three-dimensional graphics display of the initial orbit and de-orbit trajectory. Updated PDF document.
1.0.0.0