[HN Gopher] Three hours to save Integral spacecraft
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       Three hours to save Integral spacecraft
        
       Author : jensgk
       Score  : 351 points
       Date   : 2021-10-19 09:08 UTC (13 hours ago)
        
 (HTM) web link (www.esa.int)
 (TXT) w3m dump (www.esa.int)
        
       | sharmin123 wrote:
       | How to Protect Your Privacy And Personal Data from Hackers?:
       | https://www.hackerslist.co/how-to-protect-your-privacy-and-p...
        
       | xioxox wrote:
       | One of the interesting things about the telescope on Integral [1]
       | is that it uses a coded aperture mask [2] to image the sky in
       | high energy X-rays to gamma rays, rather than a focusing optic.
       | 
       | [1] https://en.wikipedia.org/wiki/INTEGRAL [2]
       | https://en.wikipedia.org/wiki/Coded_aperture
        
         | moralestapia wrote:
         | Wow, thank you for this! I had no idea such thing was possible,
         | now I'm reading a lot on it.
        
         | m4rtink wrote:
         | AFAIK thats because we dont have any usable material for X-ray
         | lenses, right ?
        
           | ncmncm wrote:
           | Used to be, they would loft a whole bunch of concentric
           | cylinders, and rely on total internal reflection off their
           | surfaces, which works even with X-rays.
           | 
           | If I understand correctly what they do now, they treat the
           | diffraction pattern from X-rays going through a mask as a
           | sort of 2-D Fourier transform, and transform it to an image
           | with the inverse transform based on the known mask. Which is
           | very clever. I don't doubt that this description glosses over
           | the actually interesting bits.
        
       | KingOfCoders wrote:
       | "Flash, I Love You! But We Only Have Fourteen Hours Left to Save
       | the Earth!"
        
       | fouc wrote:
       | Did anyone notice the amazing cookie banner?
       | 
       | 1. It offers a 'accept essential cookies' button 2. It doesn't
       | take up as much space as many other cookie banners do.
        
         | colejohnson66 wrote:
         | Re #2: Are you on a desktop/laptop? It took up a third of my
         | screen on my phone. That's not much better than others.
        
         | xboxnolifes wrote:
         | I like the accept essential cookie button, but it doesn't much
         | smaller than most banners I come across.
        
         | perihelions wrote:
         | After checking uBlock's debug log, yes, I did notice it! It is
         | ##.cc-cookies from the rulesets "Fanboy's Annoyance" and
         | "AdGuard Annoyances".
         | 
         | (To anyone unfamiliar: these "extra" rulesets ship with uBlock
         | Origin, are disabled by default, and can be toggled in the
         | "Filter lists" tab of Settings).
         | 
         | https://github.com/gorhill/uBlock/wiki/Dashboard:-Filter-lis...
        
         | jimmaswell wrote:
         | I thought "essential" cookies didn't even need consent? Either
         | way, cookie consent nonsense and the banners caused by it are a
         | blight whose benefits ("solving" the absolute non-problem of
         | advertisement tracking) pale in comparison to the enormous
         | collective inconvenience and wasted developer hours they've
         | caused us all. It's sad that we look at a banner that's not as
         | bad as it can be and appreciate it, like someone saying their
         | spouse only hit them three times today instead of ten.
        
           | fouc wrote:
           | Yeah, it's unfortunate that the bar is so low
        
       | greenail wrote:
       | These reaction wheels have such a high failure rate. Is it a
       | fundamental Tribology problem? _edit_ I see they think it was a
       | software issue but I still wonder about reaction wheel failure
       | rates.
        
         | opwieurposiu wrote:
         | One failure mode is static electricity build up leading to arc
         | discharge and pitting the bearing races. Also, the vacuum tends
         | to make the bearing grease evaporate. Back in the 60's they
         | used spermaceti, maybe we should go back to that?
         | 
         | https://est-aegis.info/2018/08/in-space-no-one-can-hear-your...
        
           | nitrogen wrote:
           | I'd wager that modern synthetic oils could beat whale oil,
           | but now I'm curious what the state of the art is.
        
         | outworlder wrote:
         | High failure rate? This particular spacecraft is 19 year old.
         | 
         | There was a string of reaction wheel failures in the past that
         | were tracked to a single supplier (forgot exactly what the
         | issue was, but I think it was some contaminant).
         | 
         | Regardless, it's a device that has to continuously spin at high
         | speeds, in space. It's actually remarkable that they survive
         | for as long as they do.
        
       | xtiansimon wrote:
       | > "Most of the Control Team were working from home at this point
       | - I was following operations from the train!"
       | 
       | The future is here!
        
         | [deleted]
        
       | thriftwy wrote:
       | I wonder why did they call it so. Either they did not know of
       | prior art[1], or knew it all too well and embraced it.
       | 
       | 1. https://en.wikipedia.org/wiki/We_(novel)
        
       | [deleted]
        
       | bjackman wrote:
       | Cool story! I wonder if the mission engineers do a lot of
       | operational training for incidents like this: for example the
       | SREs at Google do "tabletop" role-playing exercise to practice
       | incident response. Would be cool to hear similarities/differences
       | with ESA folks.
        
         | marsokod wrote:
         | There are many simulations like that when sadistic engineers
         | (sorry, simulation engineers) will inject errors in the
         | simulator and see how the operators react. Then the operators
         | have to find a way out. This is also used to make sure that
         | monitorings and procedures cover all the errors.
        
       | milgrim wrote:
       | I am surprised to read that Safe Mode did not automatically
       | disable all non essential systems. That seems to be very risky
       | behavior.
        
       | perihelions wrote:
       | This one regained spin control too late,
       | 
       | https://en.wikipedia.org/wiki/Wide_Field_Infrared_Explorer#W...
       | (1999)
        
       | trenning wrote:
       | Did the reaction wheel recover from this or is it dead? Article
       | started by saying they used 3 so now only 2 are operational? Can
       | they sustain the satellite with 2?
        
         | moffkalast wrote:
         | From what I gather it was just a radiation caused software
         | glitch that momentarily shut it down.
         | 
         | > Integral has since remained under control, and from 27
         | September all systems are back online. Since 1 October, after
         | an extended checkout, its instruments are back observing the
         | high energy Universe.
         | 
         | Seems like they're back in shape.
         | 
         | As a comparison the Kepler telescope had 4 wheels, of which 2
         | eventually completely failed and they managed to get it into a
         | neutrally stable orientation that could be managed with just
         | the two and some thruster assistance. Until RCS ran out that
         | is. 3 are generally the minimum you'd need to orient yourself
         | in 3 axis, as one might expect.
        
       | ericpauley wrote:
       | The article briefly mentions dumping energy at regular periods
       | without using thrusters. Does anyone know what mechanism they're
       | using to do this? At first glance I'd assume it would look like
       | rotating/configuring the satellite so the solar wind imparts
       | angular momentum.
        
         | jakewins wrote:
         | https://en.m.wikipedia.org/wiki/Control_moment_gyroscope
         | 
         | Perhaps? The ISS uses these.
        
         | [deleted]
        
         | Gravityloss wrote:
         | Excellent question and it turns out there's a whole article
         | about the solution!
         | https://www.esa.int/Enabling_Support/Operations/Rescuing_Int...
         | 
         | > By using a specially designed sequence of manoeuvres, the
         | control team realised they could redistribute the angular
         | momentum stored onboard the satellite using two different
         | reaction wheels spinning in opposing directions, causing the
         | spacecraft to flip.
         | 
         | > "So at this point we knew we could control the build up of
         | energy absorbed from the Sun, and christened this new manoeuvre
         | the z-flip".
        
         | techdragon wrote:
         | There's actually several small to medium effects on any
         | spacecraft in orbit around earth. There will be tiny
         | perturbations from the interaction of earths electromagnetic
         | field as it moves through it slowly, there's atmospheric drag
         | on solar panels and the spacecraft body that can create
         | "aerodynamic" torques related to what the normal orientation is
         | relative to the earth. There's even smaller perturbation from
         | the solar wind... some spacecraft have a thing (or can fudge
         | one using some part of the electrical subsystems) called a
         | "magneto-torquer" which is basically a solenoid/electromagnet
         | designed to tug on the earth's magnetic field so they can trade
         | electrical power for physical force.
         | 
         | It's a pretty cool thing that seems to be happening more and
         | more frequently with spacecraft flight dynamics teams
         | developing such a detailed model of all these forces that they
         | can invent new "stable modes" like the one they used in this
         | article, or the Kepler missions K2 mode where they found
         | another useful mode instead of just ending the mission. It's
         | not as dramatic as something like a solar sailing mission, but
         | I think it's a pretty awesome technical achievement, like
         | watching a trained stuntman drive a car on two wheels through a
         | slalom course, like a form of highly skilled, kinetic, robot
         | based gymnastics.
        
         | baybal2 wrote:
         | https://en.wikipedia.org/wiki/Tennis_racket_theorem
         | 
         | Just turn it 180 every few days this way, so the torque from
         | external influences is cancelled out.
        
           | finnh wrote:
           | The NASA video on that page is mesmerizing.
        
         | frayesto wrote:
         | I think what they are referring to is "angular momentum dumps".
         | The reaction wheels have a fixed maximum amount of angular
         | momentum. This is a function of the speed of the wheels
         | themselves since the mass/moment of inertia is fixed.
         | 
         | Over time external forces continue to add momentum to the
         | system (from drag/solar radiation pressure). In order to
         | maintain a desired pointing direction this means the wheels
         | must increase in velocity to "absorb" this momentum.
         | 
         | Eventually you need to "dump" the momentum using another
         | external force, such as thrusters, or in this case the same
         | solar radiation pressure.
         | 
         | Goal is to orient spacecraft such that external forces can be
         | used to spin down the various reaction wheels, thereby
         | "dumping" momentum out of the wheels.
         | 
         | This is pretty common on all spacecraft, but gets
         | complicated/innovative when you have to do it in an emergency
         | or if you don't have a full set of reaction wheels.
        
           | jcims wrote:
           | Just adding it because I think it's a cool use of the word.
           | When reaction wheels are operating at maximum speed and can
           | no longer exchange momentum with the spacecraft in both
           | directions, they are considered 'saturated'.
        
             | taneq wrote:
             | 'Saturated' is used in control systems engineering for any
             | value (sensor input, drive output etc.) that has reached
             | maximum or minimum value and can't be further
             | increased/decreased. It's the same sense of the word as
             | used in the HSV colour space in computer graphics.
        
         | amundsentb wrote:
         | "using its highly sensitive reaction wheels"
        
           | mcherm wrote:
           | Yes, the article uses those words. But an understanding of
           | elementary physics tells us that momentum is conserved in an
           | isolated system. Spending the reaction wheels can cause the
           | outer frame of the satellite to rotate in a certain fashion
           | but it cannot possibly alter the overall momentum or angular
           | momentum of the entire satellite unless it somehow interacts
           | with an external force.
        
             | snovv_crash wrote:
             | I guess the motors are lossy and some of it gets converted
             | to heat if they speed the wheels up and down
        
               | WJW wrote:
               | That won't solve the conservation of momentum problems
               | though, it'll just use more energy to get to the same
               | state. If you could demonstrate controlling the rotation
               | of a spacecraft just by using more inefficient motors you
               | would upend a large portion of modern physics and could
               | probably go and collect your Nobel prize within the week.
        
               | snovv_crash wrote:
               | Ok, read TFA now. It sounds like they need to dump energy
               | from the reaction wheels. Maybe they can do this by
               | inducing a spin, rotating 180 on a different axis then
               | cancelling the spin?
        
               | FeepingCreature wrote:
               | You can't cheat conservation of momentum, no matter how
               | cleverly you move your spacecraft. That's why all the
               | solutions involve expelling reaction mass. (Or, in the
               | case of solar wind, interacting with an external force.)
        
             | [deleted]
        
             | misnome wrote:
             | Right, the reaction wheels help if you want to maintain
             | orientation of the satellite under external forces that
             | want to (gently!) rotate it. And eventually your reaction
             | wheel saturates and you can't get more useful rotation out
             | of it.
             | 
             | This is where thrusters are useful, because you can use the
             | thrusters to give you a "source of force" while you spin
             | the reaction wheels back down. I believe this is where the
             | original parent's question is coming from - if you have no
             | thrusters, how do you avoid saturation?
             | 
             | Presumably, they've worked out a way to accurately predict
             | the external forces and gently operate against them while
             | spinning the wheels down in a way that doesn't make the
             | satellite spin faster.
        
               | [deleted]
        
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       (page generated 2021-10-19 23:01 UTC)