<?xml version="1.0" encoding="utf-8" standalone="yes"?><rss version="2.0" xmlns:atom="http://www.w3.org/2005/Atom"><channel><title>Spacecraft | Zhipeng Shen</title><link>https://shenzp97.github.io/ZhipengSHEN/tag/spacecraft/</link><atom:link href="https://shenzp97.github.io/ZhipengSHEN/tag/spacecraft/index.xml" rel="self" type="application/rss+xml"/><description>Spacecraft</description><generator>Hugo Blox Builder (https://hugoblox.com)</generator><language>en-us</language><lastBuildDate>Thu, 01 Jul 2021 00:00:00 +0000</lastBuildDate><image><url>https://shenzp97.github.io/ZhipengSHEN/media/icon_hu7c7ff53733ba0d22dcfb98ad8fa4fb32_37706_512x512_fill_lanczos_center_3.png</url><title>Spacecraft</title><link>https://shenzp97.github.io/ZhipengSHEN/tag/spacecraft/</link></image><item><title>Close-Approach Guidance for On-Orbit Servicing Spacecraft</title><link>https://shenzp97.github.io/ZhipengSHEN/project/spacecraft-guidance/</link><pubDate>Thu, 01 Jul 2021 00:00:00 +0000</pubDate><guid>https://shenzp97.github.io/ZhipengSHEN/project/spacecraft-guidance/</guid><description>&lt;p>During my research internship at the Beijing Institute of Spacecraft System Engineering, I investigated close-approach guidance for the rendezvous and docking of on-orbit servicing spacecraft.&lt;/p>
&lt;p>I optimized relative trajectories using the Gaussian pseudospectral method and designed an LQR guidance law for the Clohessy–Wiltshire equations. I also conducted representative mission simulations in Systems Tool Kit (STK) and analyzed guidance errors induced by measurement uncertainty.&lt;/p>
&lt;p>This work received the &lt;strong>Outstanding Intern Award&lt;/strong>.&lt;/p></description></item></channel></rss>