<?xml version="1.0" encoding="UTF-8"?><rss version="2.0"
	xmlns:content="http://purl.org/rss/1.0/modules/content/"
	xmlns:wfw="http://wellformedweb.org/CommentAPI/"
	xmlns:dc="http://purl.org/dc/elements/1.1/"
	xmlns:atom="http://www.w3.org/2005/Atom"
	xmlns:sy="http://purl.org/rss/1.0/modules/syndication/"
	xmlns:slash="http://purl.org/rss/1.0/modules/slash/"
	>

<channel>
	<title>каденцию наблюдений Archives &#8212; MATLAB Number ONE</title>
	<atom:link href="https://matlab1.com/product-tag/%d0%ba%d0%b0%d0%b4%d0%b5%d0%bd%d1%86%d0%b8%d1%8e-%d0%bd%d0%b0%d0%b1%d0%bb%d1%8e%d0%b4%d0%b5%d0%bd%d0%b8%d0%b9/feed/" rel="self" type="application/rss+xml" />
	<link>https://matlab1.com/product-tag/каденцию-наблюдений/</link>
	<description>MATLAB Simulink &#124; Tutorial &#124; Code &#124; Project</description>
	<lastBuildDate>Tue, 28 Nov 2023 19:32:46 +0000</lastBuildDate>
	<language>en-GB</language>
	<sy:updatePeriod>
	hourly	</sy:updatePeriod>
	<sy:updateFrequency>
	1	</sy:updateFrequency>
	

<image>
	<url>https://matlab1.com/wp-content/uploads/2018/08/icon1-100x100.png</url>
	<title>каденцию наблюдений Archives &#8212; MATLAB Number ONE</title>
	<link>https://matlab1.com/product-tag/каденцию-наблюдений/</link>
	<width>32</width>
	<height>32</height>
</image> 
	<item>
		<title>Orbital fit difference (D-value) and observational cadence</title>
		<link>https://matlab1.com/shop/python-code/orbital-fit-difference-d-value-observational-cadence/</link>
					<comments>https://matlab1.com/shop/python-code/orbital-fit-difference-d-value-observational-cadence/#respond</comments>
		
		<dc:creator><![CDATA[global MATLAB]]></dc:creator>
		<pubDate>Thu, 08 Feb 2018 08:36:23 +0000</pubDate>
				<guid isPermaLink="false">https://matlab1.com/?post_type=product&#038;p=4141</guid>

					<description><![CDATA[<p>Near-Earth Objects (NEOs) are orbiting bodies in near-Earth space. This can include comets, asteroids, and natural and artificial space debris. Here we are primarily concerned with asteroids in this space. These asteroids typically have small diameters and low albedo, they are very small, very dark, and difficult to observe. Since these objects exist in near-Earth space they have the [&#8230;]</p>
<p>The post <a href="https://matlab1.com/shop/python-code/orbital-fit-difference-d-value-observational-cadence/">Orbital fit difference (D-value) and observational cadence</a> appeared first on <a href="https://matlab1.com">MATLAB Number ONE</a>.</p>
]]></description>
		
					<wfw:commentRss>https://matlab1.com/shop/python-code/orbital-fit-difference-d-value-observational-cadence/feed/</wfw:commentRss>
			<slash:comments>0</slash:comments>
		
		
			</item>
	</channel>
</rss>
