Scav
Mostly Harmless
- Joined
- May 8, 2010
- Messages
- 1,002
- Reaction score
- 38
- Points
- 48
Hi guys.
Setup: Past peak heating; later stages of re-entry. I'm at between 200,000' and 150,000 feet of altitude, at a range of mach 10 and mach 9.
Symptoms: At this altitude and velocity range, vertical velocity will begin to decline rapidly at an AOA of 30-35 degrees, from an initial value of ~-300 fps. The rate of vertical velocity decay is approximately 20-60 degrees per second squared, rising exponentially over several seconds' flight time; there is little time to recognize the shift from stalled-wing flight to natural flight as my only cue to this is the multifunction HUD on the right.
Aggravating circumstances:
1. Altering attitude control from AOA-centered to pitch-centered, and forcing the nose down when the vertical velocity reaches critical decay will dramatically increase the rate of decay and 'pop' the ship into positive vertical acceleration, resulting in a 'phugoid'-like pattern in the air. This will, naturally, blast me well over the vertical path which at multi-mach flight less than two hundred miles from my destination is rather undesirable.
2. Doing nothing and maintaining a nose-high attitude will precipitate an incipient stall into an advanced stall. Do not want, especially over a patch of fake pink flamingos.
Question:
Is there a better way to mitigate the violent 'porpoising' effect I've outlined here? I've noticed the DGIV autopilot (which probably has a MUCH smaller airframe to work with) seems to have an algorithm to slowly lower the nose after a given AOA, velocity, and altitude variable. Must I mimic the same to get the desired result (a smooth transition)?
Thanks in advance.
Setup: Past peak heating; later stages of re-entry. I'm at between 200,000' and 150,000 feet of altitude, at a range of mach 10 and mach 9.
Symptoms: At this altitude and velocity range, vertical velocity will begin to decline rapidly at an AOA of 30-35 degrees, from an initial value of ~-300 fps. The rate of vertical velocity decay is approximately 20-60 degrees per second squared, rising exponentially over several seconds' flight time; there is little time to recognize the shift from stalled-wing flight to natural flight as my only cue to this is the multifunction HUD on the right.
Aggravating circumstances:
1. Altering attitude control from AOA-centered to pitch-centered, and forcing the nose down when the vertical velocity reaches critical decay will dramatically increase the rate of decay and 'pop' the ship into positive vertical acceleration, resulting in a 'phugoid'-like pattern in the air. This will, naturally, blast me well over the vertical path which at multi-mach flight less than two hundred miles from my destination is rather undesirable.
2. Doing nothing and maintaining a nose-high attitude will precipitate an incipient stall into an advanced stall. Do not want, especially over a patch of fake pink flamingos.
Question:
Is there a better way to mitigate the violent 'porpoising' effect I've outlined here? I've noticed the DGIV autopilot (which probably has a MUCH smaller airframe to work with) seems to have an algorithm to slowly lower the nose after a given AOA, velocity, and altitude variable. Must I mimic the same to get the desired result (a smooth transition)?
Thanks in advance.