I'm frankly surprised people willing to sink 15AMUs installed on these consumer grade toys are surprised by the consumer grade nature of said toys. It's not like the airspeed dependency of these "differential equation solved" attitude depictions is a state secret. The problem is that such criticism always gets cut at as socioeconomic envy. Hey man, no skin off my back; I'm not the one out 20 AMUs while getting to the same destination as the one 20Gs lighter in the wallet with two red Xs in IMC. The class envy accusations I don't have much time for though. Don't want to listen to objective criticism of these GA computer toys? Eat cake then. How's that for a class envy retort....
For the uninitiated. Attitude depictions on these all-in-one tinker toys are based on computer code that
solves for the pitch and roll values, based on
acceleration information from consumer grade MEMS accelerometers aligned in certain pre-known orientations relative to the box as-installed. Where they proceed to cheap out is in establishing the gravity vector, which is needed to "align" the solution against what can kill you. Toys like the early versions of the RCA 2600 didn't use pitot or GPS inputs at all, making it all MEMS based math, and the
precession during acceleration made my mechanical AI look like Apollo Lunar Module docking in quality. Instead, they get around that problem by using airspeed, or worse, GPS speed, to attain that fourth and "caging" variable. Problem is that now No speed means no gonk, means no fancy display, means a red-X four fingers shy of a high-five for you when the chips are down. Oops. Guess ripping out that brass pneumatic AI wasn't such a hot idea after all.
For those who don't fly behind toys, the electronic depictions of attitude are based on no-kidding
ring laser gyros that provide
direct angle rate information in all three axis by measuring frequency interference of two counter-propagating laser signals (Sagnac effect). Which means, for those keeping track, no airspeed data is needed to provide
direct attitude solution. Furthermore, GPS info is used to only update the nav position of the ship, aiding the accelerometers portion of the INS to keep nav position integrity. Not that it needs much after initial alignment, especially in short duration flights. Though airspeed information is embedded into the ADC on most of these INS solutions, loss of airspeed data means Rick-all to the attitude depiction. This is what airliners and birds of killing alike fly behind, and not your Toys-R-Us
accelerometer-based Aspen/G5/Dynon.
Even mechanical brass has vanes that inherently point at the gravity vector in order to divert pneumatics and re-cage the presentation card in front of the gyro. Aspen doesn't even have the electronic version of that, which is what it would otherwise need in order to not necessitate airspeed to solve the equations for roll and pitch without a crutch.
So to reiterate. When you buy a garmin/aspen box, you're not buying a RLG. As such you should consider the manner and severity of conditions in which you launch without a robust attitude information backup. I personally would prefer a brass gyro for a backup, but Needle-ball-airspeed is legal too I suppose. Though the latter is ill advised for the weekend warrior imo, if the stats that led to AC 91-75 are to be taken at face value.