https://www.aero.iitb.ac.in/satelliteWiki/index.php?action=history&feed=atom&title=Requirements_on_ADCS_by_other_SubsystemsRequirements on ADCS by other Subsystems - Revision history2026-09-10T20:23:42ZRevision history for this page on the wikiMediaWiki 1.30.0https://www.aero.iitb.ac.in/satelliteWiki/index.php?title=Requirements_on_ADCS_by_other_Subsystems&diff=1309&oldid=prevYash at 10:23, 23 February 20182018-02-23T10:23:20Z<p></p>
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<tr><td class='diff-marker'> </td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>#The communication subsystem will require the antennae to point in a particular direction for proper communication, which will place constraints on satellite attitude.  </div></td><td class='diff-marker'> </td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>#The communication subsystem will require the antennae to point in a particular direction for proper communication, which will place constraints on satellite attitude.  </div></td></tr>
<tr><td class='diff-marker'> </td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>#In general, the angular rates of the satellite need to be within a particular threshold for proper operation of the payload and proper communication between the satellite and the ground station.<br \></div></td><td class='diff-marker'> </td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>#In general, the angular rates of the satellite need to be within a particular threshold for proper operation of the payload and proper communication between the satellite and the ground station.<br \></div></td></tr>
<tr><td colspan="2"> </td><td class='diff-marker'>+</td><td style="color:black; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;">----</ins></div></td></tr>
<tr><td class='diff-marker'> </td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>If you are done reading this page, you can go back to [[Attitude Determination and Control Subsystem]]</div></td><td class='diff-marker'> </td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>If you are done reading this page, you can go back to [[Attitude Determination and Control Subsystem]]</div></td></tr>
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</table>Yashhttps://www.aero.iitb.ac.in/satelliteWiki/index.php?title=Requirements_on_ADCS_by_other_Subsystems&diff=91&oldid=prevAdmin: Protected "Requirements on ADCS by other Subsystems" ([Edit=Allow only autoconfirmed users] (indefinite) [Move=Allow only autoconfirmed users] (indefinite))2018-01-19T19:13:27Z<p>Protected "<a href="/satelliteWiki/index.php/Requirements_on_ADCS_by_other_Subsystems" title="Requirements on ADCS by other Subsystems">Requirements on ADCS by other Subsystems</a>" ([Edit=Allow only autoconfirmed users] (indefinite) [Move=Allow only autoconfirmed users] (indefinite))</p>
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</td></tr></table>Adminhttps://www.aero.iitb.ac.in/satelliteWiki/index.php?title=Requirements_on_ADCS_by_other_Subsystems&diff=67&oldid=prevYash at 09:49, 19 January 20182018-01-19T09:49:11Z<p></p>
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<td colspan="2" style="background-color: white; color:black; text-align: center;">Revision as of 09:49, 19 January 2018</td>
</tr><tr><td colspan="2" class="diff-lineno" id="mw-diff-left-l2" >Line 2:</td>
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<tr><td class='diff-marker'> </td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>#Satellite attitude needs to be maintained for reception of a sufficient amount of solar flux to generate power. If solar panels are fixed, then the satellite attitude will directly influence the solar flux received. If solar panels are deployable, their orientation will need to be controlled for optimum power generation. Even in this case, the attitude will affect the solar flux received.</div></td><td class='diff-marker'> </td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>#Satellite attitude needs to be maintained for reception of a sufficient amount of solar flux to generate power. If solar panels are fixed, then the satellite attitude will directly influence the solar flux received. If solar panels are deployable, their orientation will need to be controlled for optimum power generation. Even in this case, the attitude will affect the solar flux received.</div></td></tr>
<tr><td class='diff-marker'> </td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>#The communication subsystem will require the antennae to point in a particular direction for proper communication, which will place constraints on satellite attitude.  </div></td><td class='diff-marker'> </td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>#The communication subsystem will require the antennae to point in a particular direction for proper communication, which will place constraints on satellite attitude.  </div></td></tr>
<tr><td class='diff-marker'>−</td><td style="color:black; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;"><div>#In general, the angular rates of the satellite need to be within a particular threshold for proper operation of the payload and proper communication between the satellite and the ground station.</div></td><td class='diff-marker'>+</td><td style="color:black; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div>#In general, the angular rates of the satellite need to be within a particular threshold for proper operation of the payload and proper communication between the satellite and the ground station.<ins class="diffchange diffchange-inline"><br \></ins></div></td></tr>
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</table>Yashhttps://www.aero.iitb.ac.in/satelliteWiki/index.php?title=Requirements_on_ADCS_by_other_Subsystems&diff=66&oldid=prevYash: Created page with "#The payload can require the satellite to maintain certain attitude for success. For example, an imaging payload can require the imager to point towards the object which it is..."2018-01-19T09:44:06Z<p>Created page with "#The payload can require the satellite to maintain certain attitude for success. For example, an imaging payload can require the imager to point towards the object which it is..."</p>
<p><b>New page</b></p><div>#The payload can require the satellite to maintain certain attitude for success. For example, an imaging payload can require the imager to point towards the object which it is imaging, which will place constraints on the attitude. <br />
#Satellite attitude needs to be maintained for reception of a sufficient amount of solar flux to generate power. If solar panels are fixed, then the satellite attitude will directly influence the solar flux received. If solar panels are deployable, their orientation will need to be controlled for optimum power generation. Even in this case, the attitude will affect the solar flux received.<br />
#The communication subsystem will require the antennae to point in a particular direction for proper communication, which will place constraints on satellite attitude. <br />
#In general, the angular rates of the satellite need to be within a particular threshold for proper operation of the payload and proper communication between the satellite and the ground station.</div>Yash