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Feb 28, 2021 at 6:39 vote accept zephyr0110
Dec 18, 2018 at 0:33 answer added Steve Linton timeline score: 1
Dec 17, 2018 at 10:10 comment added Steve Linton Gravity Probe B en.wikipedia.org/wiki/Gravity_Probe_B sensed its attitude relative to IM Pegasi (whose own absolute position was measured relative to distant quasars by Earth-based radio astronomy). More details einstein.stanford.edu/TECH/technology1.html#telescope. Pointing accuracy was < 0.1 milliarcseconds (about 0.5 nanoradians).
Dec 17, 2018 at 4:51 answer added uhoh timeline score: 0
Apr 18, 2018 at 13:34 answer added uhoh timeline score: 4
Apr 9, 2018 at 3:26 history tweeted twitter.com/StackSpaceExp/status/983184260415844355
Apr 9, 2018 at 2:48 answer added David Hammen timeline score: 7
Apr 9, 2018 at 1:06 history edited zephyr0110 CC BY-SA 3.0
deleted 165 characters in body
Apr 9, 2018 at 1:05 comment added zephyr0110 But, I just put that as an example that why would someone want this high degree accuracy. I shall research a bit on high bandwidth optical communication. Though, still the core issue remains same, the misalignment measured by conventional attitude sensors are poor for such endeavor spare the hubble I guess.
Apr 8, 2018 at 23:47 comment added uhoh So I'm just suggesting that it might be better to completely separate one question about precision attitude control from another question about sub-arcsec pointing of optical communication.
Apr 8, 2018 at 23:45 comment added uhoh @Prakhar a small unit placed at the focal plane can contain both a light emitter (fiber pigtail attached to a laser diode+modulator) and a CCD monitoring positions of stars, planets, or other objects within a degree or so of the target which may be invisible. A computer + ephemeris will know the orientation of one with respect to the other, and be able to do the light time and other corrections. If image processing detects a misalignment, tiny MEMS actuators can move the FP unit, or just the fiber by microns in order to compensate. No need to change the attitude of the whole spacecraft.
Apr 8, 2018 at 21:38 comment added zephyr0110 But in order to steer the optical component one needs the knowledge of where to steer. How can that be possibly done without attitude knowledge?
Apr 8, 2018 at 20:15 comment added uhoh This is because light is really quite slow, and in space everything is moving, and correcting the direction of a beam of light can be done with small optical components much more easily and precisely than trying to control the attitude of the entire spacecraft, since it's not really a rigid body at all at this level
Apr 8, 2018 at 18:58 comment added uhoh Rigid body rotation with respect to a hypothetical absolutely inertial frame is one question, generating an optical wave front that will maximize signal strength when it is ultimately received at a distant location is quite another. Both have general relativity implications but the second one is best done without thinking about the first. If you really want to ask about pointing a sub-arcsec resolving optical system to maximized a distance received signal strength, it's better to ask that without bringing up anything about spacecraft attitude or inertial frames.
Apr 8, 2018 at 17:13 history edited zephyr0110 CC BY-SA 3.0
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Apr 8, 2018 at 16:22 comment added zephyr0110 That is exactly my question. Even if one considers star as reference in a different galaxy. One simply does not have enough accurate sensor to get the attitude of the star as of now. Now, I want to make an object truly non-rotating. Probably, aligning it to perfect attitude would be next level of challenge.
Apr 8, 2018 at 16:11 comment added fred_dot_u when considering a rotation, one has a reference datum. In your question, what is the reference point? A remote star would provide a reference point at a galactic level, wouldn't it? The galaxy rotates too!
Apr 8, 2018 at 15:32 history asked zephyr0110 CC BY-SA 3.0