Thanks!
I'll share one piece of information. The attached graph is the correction the system made in the 3 stage flight (correcting from nominally 6° to about 1.5°. That made a big difference in the recovery distance. One thing that I have learned is that the canards create quite a bit of torque on the air frame. The oscillations in the tilt in the graph are due to air frame flexing and not changes in the control. On my test rocket, I applied carbon to a fiberglass aif frame to try to limit that bending, and the torgue can prevent parts of the rocket from separating. This issue would likely prevent the use of my three-stage approach on a weak rocket - there just isn't enough time in a coast to make a significant change in direction. If canards were used at the top of a weak rocket, it would be necessary to use small canards and small control actions to avoid tearing up the air frame. The idea would be to just keep slowly working back towards vertical over a long period. But, there is the weight penalty of keeping a system attached for an entire flight.
I did the two-stage flight in the video below a few years back. The stabilization system was on top of the rocket. The flight was two M motors, but the velocity was below Mach 1 for the entire flight. It only went to 23K though, and it's really hard to envision how to scale this up to 100K. Incidently, you can see the air frame flex I mentioned in the video (before I applied carbon to the rocket). That would be a real problem for a weak rocket.
Jim
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