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👥 Mandatory Attendees
Name | Phone # | Role | Reason |
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Flight Test Lead |
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Pilot in Command |
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Safety |
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(Subsystems integration, Secondary pilot, etc) |
👥 Auxilliary Attendees
Name | Role |
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Yuchen Lin Jerry Tian bootcamper: Hanwu, and one more uhh forgot his name | |
🥅 Goals/Objectives
Objective ALL PROGRAMS RUN IN ACRO | Priority | Owner(s) |
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0-25-0 ramp
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0-50-0 Step
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0-100-0 Step
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0-100-hold 5 seconds-0
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sine wave ramping
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Flight Test Debrief
Flight Test Timeline
Step up:
This morning, we found out the Tbs nano receiver(white) that was originally placed on the drone might be broken (not status light with power). We replaced it with the receiver from Houston.
Radio Control, accelerometer, and compass calibrated for Pegasus by mission planner
No telemetry connection while testing, only radio control
ratchet strap fixed the drone on the table of E7 1401
Observation:
After arming, the props spin up on their own. The airframe vibrates slightly under the initial low throttle. The vibration could be caused due to the landing gear connection and the flexibility of the arms. Not a big issue in my opinion since the airframe restores a stable state after giving the motor some throttle, and it fixes itself.
No obvious problem was noticed as the throttle slowly went from 0 - 50% and went back.
No obvious problem as the throttle quickly went to 100% and stopped.
Didn’t check throttle stays on 100% for 5 seconds or sine wave ramp
Analytics (hopefully applicable)
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Child pages (Children Display) |
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Action Items
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