^^^^^ Thanks for the info for us, the great unwashed.![]()
I understand, but this is the oddest sentence to get used to...![]()
The electric jet knows all. Hal is flying.
The Rhino is even more departure resistant than the legacy Hornet.
^^^^^ Thanks for the info for us, the great unwashed.![]()
I understand, but this is the oddest sentence to get used to...![]()
The electric jet knows all. Hal is flying.
The Rhino is even more departure resistant than the legacy Hornet.
That, in all honesty would spook me (maybe having an ejection seat would help a bit)
The 60's have a Computer, but you can override and fly without it..
UInavy said:Watch the control surfaces on any type of Hornet while its in the groove. The frequency and amount of control deflections being made by the FCS are amazing. The stick still produces the desired output (houses get bigger/smaller), the FCS just firgures out the most efficient way for that to happen. While overriding the computer is possible, its not recommended. Nothing to do with an ejection seat, thats just the way the system works. It can fix a spin quicker than anti-spin inputs can do it. That way, you're further from the deck and pants don't get quite as stained.
I thought your computers were run on reel to reel tapes.......
controls release/feet off rudders/speedbreak in
still out of control:
throttles - idle
altitude, AOA, airspeed, yaw rate - check
when recovery is indicated by AOA & yaw rate tones removed, side forces subsided, airspeed accelerating above 180 knots - recover
passing 6000 feet AGL dive recovery not initiated - eject
So heres a question.
With some of the photos taken of aircraft currently operating in the Sandbox they seem to have a lot of asymetrical loads being a common place thing. How does that effect recovery checklists or overall recoverability its self?
interesting ... thanks for the heads up.changed in november to mimic the rhino bretheren and makes use of the spin rec switch a thing of the past with the new software
controls release/feet off rudders/speedbreak in
still out of control:
throttles - idle
altitude, AOA, airspeed, yaw rate - check
if command arrow present - lat stick full with arrow
when command arrow removed - lat stick smoothly neutral
when recovery is indicated by AOA & yaw rate tones removed, side forces subsided, airspeed accelerating above 180 knots - recover
passing 6000 feet AGL dive recovery not initiated - eject
fuselage fuel leak not boldface now either. other minor changes...
it's a CRAZY new world we live in gents![]()
UInavy said:Yep. In a fully developed spin, all the displays will display a 'command arrow' indicating which way to fully deflect the stick, as it may not be obvious in a strange situation (such as the falling leaf.)
maybe this is a dumb question, but considering the computer can (from how it sounds) pretty much do what it wants, why even include pilot inputs into the recovery? (i.e why doesn't the jet just deflect the stick for you?)
maybe this is a dumb question, but considering the computer can (from how it sounds) pretty much do what it wants, why even include pilot inputs into the recovery? (i.e why doesn't the jet just deflect the stick for you?)
OCF procedures for the "classic" hornet, such as the one in the video ...
controls release/feet off rudders/speedbreak in
still out of control:
throttles - idle
altitude, AOA, airspeed, yaw rate - check
when recovery is indicated by AOA & yaw rate tones removed, side forces subsided, airspeed accelerating above 180 knots - recover
passing 6000 feet AGL dive recovery not initiated - eject