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What exactly is Rhumb-line control in the context of a launch trajectory?


If there “won't be” rockets to launch individual cubesats, then why did JAXA build exactly that? (SS-520-xx)How do small, spin stabilized launchers follow a Rhumb line?The Russians recently tested a new launch trajectory that goes to the space station in about six hours. What allowed for the difference?How does a launch vehicle control its trajectory during the first stage?Why don't some rockets launch in a straight line?What is the maximum acceptable latency in rocket control computers?What is the basic optimal trajectory for a launch vehicle?What are possible trajectory azimuths at Wallops?How and where can I determine the direction of a launch prior to liftoff?For an Apollo Lunar Module Ascent Stage launch, what is the optimal profile of $beta$ (or $gamma$) vs time?Most preferred coordinate system for Launch vehicle trajectoryIs there a pitch maneuver in launch vehicle trajectory to raise the perigee altitude in order to circularize?






.everyoneloves__top-leaderboard:empty,.everyoneloves__mid-leaderboard:empty,.everyoneloves__bot-mid-leaderboard:empty margin-bottom:0;








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$begingroup$


The conference paper SS-520 Nano satellite launcher and its flight result SSC18-IX-03 from the 32nd Annual AIAA/USU Conference on Small Satellites linked in this answer describes the use of Rhumb-line control in several places.



If I look at Wikipedia's Rhumb line it is a mathematical concept, and I don't see how it would apply to a normal launch to orbit trajectory:




In navigation, a rhumb line, rhumb, or loxodrome is an arc crossing all meridians of longitude at the same angle, that is, a path with constant bearing as measured relative to true or magnetic north.




enter image description here



Question: What exactly is "Rhumb-line control" in the context of a launch to orbit trajectory? How does the use of the term reconcile with the definition in Wikipedia?




Images from the linked paper, where is the Rhumb line?



enter image description here



enter image description here










share|improve this question











$endgroup$




















    1












    $begingroup$


    The conference paper SS-520 Nano satellite launcher and its flight result SSC18-IX-03 from the 32nd Annual AIAA/USU Conference on Small Satellites linked in this answer describes the use of Rhumb-line control in several places.



    If I look at Wikipedia's Rhumb line it is a mathematical concept, and I don't see how it would apply to a normal launch to orbit trajectory:




    In navigation, a rhumb line, rhumb, or loxodrome is an arc crossing all meridians of longitude at the same angle, that is, a path with constant bearing as measured relative to true or magnetic north.




    enter image description here



    Question: What exactly is "Rhumb-line control" in the context of a launch to orbit trajectory? How does the use of the term reconcile with the definition in Wikipedia?




    Images from the linked paper, where is the Rhumb line?



    enter image description here



    enter image description here










    share|improve this question











    $endgroup$
















      1












      1








      1





      $begingroup$


      The conference paper SS-520 Nano satellite launcher and its flight result SSC18-IX-03 from the 32nd Annual AIAA/USU Conference on Small Satellites linked in this answer describes the use of Rhumb-line control in several places.



      If I look at Wikipedia's Rhumb line it is a mathematical concept, and I don't see how it would apply to a normal launch to orbit trajectory:




      In navigation, a rhumb line, rhumb, or loxodrome is an arc crossing all meridians of longitude at the same angle, that is, a path with constant bearing as measured relative to true or magnetic north.




      enter image description here



      Question: What exactly is "Rhumb-line control" in the context of a launch to orbit trajectory? How does the use of the term reconcile with the definition in Wikipedia?




      Images from the linked paper, where is the Rhumb line?



      enter image description here



      enter image description here










      share|improve this question











      $endgroup$




      The conference paper SS-520 Nano satellite launcher and its flight result SSC18-IX-03 from the 32nd Annual AIAA/USU Conference on Small Satellites linked in this answer describes the use of Rhumb-line control in several places.



      If I look at Wikipedia's Rhumb line it is a mathematical concept, and I don't see how it would apply to a normal launch to orbit trajectory:




      In navigation, a rhumb line, rhumb, or loxodrome is an arc crossing all meridians of longitude at the same angle, that is, a path with constant bearing as measured relative to true or magnetic north.




      enter image description here



      Question: What exactly is "Rhumb-line control" in the context of a launch to orbit trajectory? How does the use of the term reconcile with the definition in Wikipedia?




      Images from the linked paper, where is the Rhumb line?



      enter image description here



      enter image description here







      launch trajectory navigation flight-control launch-trajectories






      share|improve this question















      share|improve this question













      share|improve this question




      share|improve this question








      edited 7 hours ago







      uhoh

















      asked 8 hours ago









      uhohuhoh

      48.4k22 gold badges195 silver badges631 bronze badges




      48.4k22 gold badges195 silver badges631 bronze badges























          1 Answer
          1






          active

          oldest

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          3












          $begingroup$

          “Sailing a rhumb line” means holding a constant compass bearing. For short distances, this stays close to a great circle path.But at longer distances and/or higher inclinations, the rhumb-line path “tends north” of a great circle as shown in the Questions globular image.



          For a fast, short launch, a rhumb-line trajectory has the advantage of simplicity. As seen in Organic Marble’s (now deleted) answer, you can steer a constant bearing with a very simple guidance system that rides a constant bearing from the Sun (not quite a rhumb line, the Sun moves a bit, but see below)



          How non-optimal is the rhumb line path? First, note that orbital ground tracks aren’t quite great circles, as the orbiting body “tends west” as Earth turns east under the orbit. Until the rhumb line course has gone a long way north, the first part of it matches an orbital ground track pretty well.



          The specific example of indexing off the Sun’s bearing is a slight improvement, as the Sun is also “heading west” as seen from the launcher so its bearing stays aligned with the initial part of an orbital path.






          share|improve this answer











          $endgroup$














          • $begingroup$
            There's a lot happening in your answer that I've got to think about, but the first sentence sums it up nicely. The target "compass bearing" was chosen probably close to zero (East) so that the inclination was roughly equal to the launch latitude. But I'm still stuck trying to understand what "...as the error is in the helpful direction" means.
            $endgroup$
            – uhoh
            7 hours ago







          • 1




            $begingroup$
            Tried to clean up the text a bit. It was a bit confusing as it wasn’t using consistent language about what was east/west of what.
            $endgroup$
            – Bob Jacobsen
            7 hours ago













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          1 Answer
          1






          active

          oldest

          votes









          active

          oldest

          votes






          active

          oldest

          votes









          3












          $begingroup$

          “Sailing a rhumb line” means holding a constant compass bearing. For short distances, this stays close to a great circle path.But at longer distances and/or higher inclinations, the rhumb-line path “tends north” of a great circle as shown in the Questions globular image.



          For a fast, short launch, a rhumb-line trajectory has the advantage of simplicity. As seen in Organic Marble’s (now deleted) answer, you can steer a constant bearing with a very simple guidance system that rides a constant bearing from the Sun (not quite a rhumb line, the Sun moves a bit, but see below)



          How non-optimal is the rhumb line path? First, note that orbital ground tracks aren’t quite great circles, as the orbiting body “tends west” as Earth turns east under the orbit. Until the rhumb line course has gone a long way north, the first part of it matches an orbital ground track pretty well.



          The specific example of indexing off the Sun’s bearing is a slight improvement, as the Sun is also “heading west” as seen from the launcher so its bearing stays aligned with the initial part of an orbital path.






          share|improve this answer











          $endgroup$














          • $begingroup$
            There's a lot happening in your answer that I've got to think about, but the first sentence sums it up nicely. The target "compass bearing" was chosen probably close to zero (East) so that the inclination was roughly equal to the launch latitude. But I'm still stuck trying to understand what "...as the error is in the helpful direction" means.
            $endgroup$
            – uhoh
            7 hours ago







          • 1




            $begingroup$
            Tried to clean up the text a bit. It was a bit confusing as it wasn’t using consistent language about what was east/west of what.
            $endgroup$
            – Bob Jacobsen
            7 hours ago















          3












          $begingroup$

          “Sailing a rhumb line” means holding a constant compass bearing. For short distances, this stays close to a great circle path.But at longer distances and/or higher inclinations, the rhumb-line path “tends north” of a great circle as shown in the Questions globular image.



          For a fast, short launch, a rhumb-line trajectory has the advantage of simplicity. As seen in Organic Marble’s (now deleted) answer, you can steer a constant bearing with a very simple guidance system that rides a constant bearing from the Sun (not quite a rhumb line, the Sun moves a bit, but see below)



          How non-optimal is the rhumb line path? First, note that orbital ground tracks aren’t quite great circles, as the orbiting body “tends west” as Earth turns east under the orbit. Until the rhumb line course has gone a long way north, the first part of it matches an orbital ground track pretty well.



          The specific example of indexing off the Sun’s bearing is a slight improvement, as the Sun is also “heading west” as seen from the launcher so its bearing stays aligned with the initial part of an orbital path.






          share|improve this answer











          $endgroup$














          • $begingroup$
            There's a lot happening in your answer that I've got to think about, but the first sentence sums it up nicely. The target "compass bearing" was chosen probably close to zero (East) so that the inclination was roughly equal to the launch latitude. But I'm still stuck trying to understand what "...as the error is in the helpful direction" means.
            $endgroup$
            – uhoh
            7 hours ago







          • 1




            $begingroup$
            Tried to clean up the text a bit. It was a bit confusing as it wasn’t using consistent language about what was east/west of what.
            $endgroup$
            – Bob Jacobsen
            7 hours ago













          3












          3








          3





          $begingroup$

          “Sailing a rhumb line” means holding a constant compass bearing. For short distances, this stays close to a great circle path.But at longer distances and/or higher inclinations, the rhumb-line path “tends north” of a great circle as shown in the Questions globular image.



          For a fast, short launch, a rhumb-line trajectory has the advantage of simplicity. As seen in Organic Marble’s (now deleted) answer, you can steer a constant bearing with a very simple guidance system that rides a constant bearing from the Sun (not quite a rhumb line, the Sun moves a bit, but see below)



          How non-optimal is the rhumb line path? First, note that orbital ground tracks aren’t quite great circles, as the orbiting body “tends west” as Earth turns east under the orbit. Until the rhumb line course has gone a long way north, the first part of it matches an orbital ground track pretty well.



          The specific example of indexing off the Sun’s bearing is a slight improvement, as the Sun is also “heading west” as seen from the launcher so its bearing stays aligned with the initial part of an orbital path.






          share|improve this answer











          $endgroup$



          “Sailing a rhumb line” means holding a constant compass bearing. For short distances, this stays close to a great circle path.But at longer distances and/or higher inclinations, the rhumb-line path “tends north” of a great circle as shown in the Questions globular image.



          For a fast, short launch, a rhumb-line trajectory has the advantage of simplicity. As seen in Organic Marble’s (now deleted) answer, you can steer a constant bearing with a very simple guidance system that rides a constant bearing from the Sun (not quite a rhumb line, the Sun moves a bit, but see below)



          How non-optimal is the rhumb line path? First, note that orbital ground tracks aren’t quite great circles, as the orbiting body “tends west” as Earth turns east under the orbit. Until the rhumb line course has gone a long way north, the first part of it matches an orbital ground track pretty well.



          The specific example of indexing off the Sun’s bearing is a slight improvement, as the Sun is also “heading west” as seen from the launcher so its bearing stays aligned with the initial part of an orbital path.







          share|improve this answer














          share|improve this answer



          share|improve this answer








          edited 7 hours ago

























          answered 7 hours ago









          Bob JacobsenBob Jacobsen

          7,56016 silver badges37 bronze badges




          7,56016 silver badges37 bronze badges














          • $begingroup$
            There's a lot happening in your answer that I've got to think about, but the first sentence sums it up nicely. The target "compass bearing" was chosen probably close to zero (East) so that the inclination was roughly equal to the launch latitude. But I'm still stuck trying to understand what "...as the error is in the helpful direction" means.
            $endgroup$
            – uhoh
            7 hours ago







          • 1




            $begingroup$
            Tried to clean up the text a bit. It was a bit confusing as it wasn’t using consistent language about what was east/west of what.
            $endgroup$
            – Bob Jacobsen
            7 hours ago
















          • $begingroup$
            There's a lot happening in your answer that I've got to think about, but the first sentence sums it up nicely. The target "compass bearing" was chosen probably close to zero (East) so that the inclination was roughly equal to the launch latitude. But I'm still stuck trying to understand what "...as the error is in the helpful direction" means.
            $endgroup$
            – uhoh
            7 hours ago







          • 1




            $begingroup$
            Tried to clean up the text a bit. It was a bit confusing as it wasn’t using consistent language about what was east/west of what.
            $endgroup$
            – Bob Jacobsen
            7 hours ago















          $begingroup$
          There's a lot happening in your answer that I've got to think about, but the first sentence sums it up nicely. The target "compass bearing" was chosen probably close to zero (East) so that the inclination was roughly equal to the launch latitude. But I'm still stuck trying to understand what "...as the error is in the helpful direction" means.
          $endgroup$
          – uhoh
          7 hours ago





          $begingroup$
          There's a lot happening in your answer that I've got to think about, but the first sentence sums it up nicely. The target "compass bearing" was chosen probably close to zero (East) so that the inclination was roughly equal to the launch latitude. But I'm still stuck trying to understand what "...as the error is in the helpful direction" means.
          $endgroup$
          – uhoh
          7 hours ago





          1




          1




          $begingroup$
          Tried to clean up the text a bit. It was a bit confusing as it wasn’t using consistent language about what was east/west of what.
          $endgroup$
          – Bob Jacobsen
          7 hours ago




          $begingroup$
          Tried to clean up the text a bit. It was a bit confusing as it wasn’t using consistent language about what was east/west of what.
          $endgroup$
          – Bob Jacobsen
          7 hours ago

















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