Hi Grant,
Thanks for that - I hadn't realised you'd already asked people about it.
I thought there would be a process like that for the CAA, similar to the
safety cases for tests or modifications on the railway. It's been a while since
I was involved in those. The other thing I'd imagine might be an issue is what
they class it as - does having steering and a glide angle turn it into a UAV
that has a whole other set of rules to follow? I know there's been at least
one balloon launched glider controlled by ardupilot, but that was a few years
ago now and rules around drones have changed I think. It's worth finding out
about this early though - it could be a blocker to the whole idea.
I agree on the need for testing. I'd expect this to be developed as a multi-
stage thing in parallel with the balloon side, considered for use only when
we've got enough data to have confidence in it. That would include:
* tests as a kite - to demonstrate stability, tune bridling, measure lift /
drag ratio and get an idea of the range of control input needed for steering.
* drop tests from kite or drone - to test deployment, static steering trim,
descent rate at low altitude etc.
* perhaps fly it as a paramotor under remote control or via ardupilot
I hadn't thought about using rockets for testing, and have no idea about the
rules around them. It might be a viable way of getting enough altitude to test
the guidance though. My kite use is with ~30m lines, so not a lot of altitude
to play with.
So far as making a case to the CAA, it's not a novel parachute design which
should make things easier. I'd avoid mentioning kites at all - it was
originally designed and tested as a parachute.
* Apart from NASA's research there's the model rocketry use, and there's at
least one manufacturer selling them as a fully approved backup parachute for
paragliders.
* The rocketry usage gives descent rate calcs for similar size and loading,
which we should be able to back up with drop test results.
* With static trim for a steady circling it would descend in a similar path to
a conventional circular parachute sized for that descent rate.
* Deployment would be from an unpacked state, as for the conventional circular
parachute in balloon use. That's pretty much a best case scenario.
It would be good to know the rules on descent rate - with a glide angle our
absolute velocity will be significantly greater than the descent rate, so we'd
need to know which it s we need to limit. Having said that, we're almost
certain to be both slower and softer than the glider they've allowed before.
Initial use on a balloon would be passive, with the steering fixed for gentle
circling. That makes it low risk with a path similar to a round parachute, and
we get to see how it deploys and performs without worrying about issues in an
active control system. I'd want to have a video camera pointing up at the
parachute to see what it did at altitude here, as it's not something we could
test easily.
For active control I'd aim to limit turn rate by limiting the range of control
input to something we know is ok if permanently applied. If the steering gets
jammed to one side it would circle down as in the passive case, and the
control system would be set to have this as its fail safe state. Being able to
aim for an unpopulated area can't really be any worse than no control can it?
These are of course the expectations without having built or tested anything -
things WILL change!
On Wednesday, 6 September 2017 21:05:45 BST 'grant gibson' via Derby Makers
wrote: