I've successfully hand-flown reasonably physics-realistic simulations of the Shuttle in the 'orbiter' program with a few instruments. From what I've seen, provided a vehicle is attitudinally stable, and you have an artificial horizon, it's hard, but not stupidly hard; you just have to fly a certain lean over and thrust schedule until you reach orbit. Flying to orbit is not like trying to hover, an error of a few m/s or even a few hundred m/s may not stop you reaching A stable orbit, but in hover it will kill you stone dead. On 9 October 2013 20:00, Henry Spencer <henry@xxxxxxxxxxxxxxx> wrote: > On Wed, 9 Oct 2013, Ian Garcia wrote: > > > They tried it in simulation, discovered that it worked surprisingly > > > well, and decided it was worth having. > > > > Worked surprisingly well? Where is this documented? I always > > understood that it barely worked and often failed, but I admit I may > > have understood it wrong. > > I've seen mention of it several places; the one specific reference a quick > look turned up is NASA TN D-5261, "A detailed study of manual backup > control > systems for the Saturn V launch vehicle", Hardy et al. (No, alas, I don't > have a copy, just some notes from reading it.) > > It also occurs to me that "surprisingly well" is relative to one's > expectations, and isn't necessarily incompatible with "barely worked". :-) > > As has been noted in some other connections, the sheer *size* of the > Saturn V worked in favor of such things, by slowing down its responses. > > Henry Spencer > > henry@xxxxxxxxxxxxxxx > ( > hspencer@xxxxxxxxxxxxx) > ( > regexpguy@xxxxxxxxx) > > > -- -Ian Woollard