A field team faces an unresolved physical question: Why can 87 seconds consume 102 equivalent seconds? They must answer it before changing hover ratio on the real device. Predict the direction first.
See the relationship before changing it
The figure reads from left to right. The blue card is hover ratio. The middle card applies this page's relationship. The green card is time-only use. Walk the arrows once: set the input, apply the rule, then read the result with its unit.
The retained audit below checks several chapter fixtures. This added model holds every other chapter fixture fixed, so the numeric fixture does not switch without explanation.
Derive the baseline in four named moves
- 1
Name the input. The chapter baseline for hover ratio is 1.3.
- 2
Name the relationship. time-only=4.83%; teq=tflight+ρthover; used=100teq/Tbattery ρ=1.3: teq=102 s; used=5.67%; uplift=17.24%; pack sag=0.900 V
- 3
Substitute the chapter fixture. Set hover ratio to 1.3. The page ledger gives time-only use as 4.83%.
- 4
Read the result. Keep % beside the value. Use it only inside the technical boundary on this page.
Predict, then change hover ratio
Try Predict the direction of time-only use. Move one control, calculate, then check your prediction.
Observe Hover seconds count more because the model assigns them more current. More stops therefore consume reserve faster than raw mission time suggests. Reset the control to 1.3 and compare time-only use.
Explain Only hover ratio moves here. The other chapter fixtures remain fixed.
Check yourself
What should you do before trusting a moved-control result?
What does this small model leave out?
1. Start with the physical question
Replace a time-additive mission check with a current-weighted one. A reserve check that exposes hover-heavy missions.
2. Name every algebra move
Keep flight and hover separateDo not add unlike current states yet.
Choose a reference currentLet cruise current be 1 unit.
Weight hover timeMultiply hover seconds by ρ=Ihover/Icruise.
Add equivalent secondsteq=tflight+ρthover.
Compare with the reference budgetused=100teq/Tbattery.
3. Reproduce the chapter case
ρ=1.3: teq=102 s; used=5.67%; uplift=17.24%; pack sag=0.900 V
The arithmetic reproduces the chapter case while keeping its assumptions explicit.
4. Try the controlling input
TryMove the control and watch every displayed result come from the shown formula.
ObserveAt 1.30× hover current, the mission becomes 102.00 equivalent seconds and uses 5.67%, rather than the time-only 4.83%.
ExplainHover seconds count more because the model assigns them more current. More stops therefore consume reserve faster than raw mission time suggests.
This compact engine isolates one relationship; it is not a deployment certificate.
- Airframe
- The 1.3 ratio is illustrative and changes with mass, speed, wind, and propellers
- Battery
- The 1800 s reference is not a complete discharge curve
- Mission
- Climb, acceleration, payload, reserve policy, and weather are omitted
Measure the real system and reopen the decision when its inputs change.
5. Measure the mission states
Log current during takeoff, cruise, hover, climb, descent, payload work, and landing. Integrate those samples and preserve the operational reserve.
6. Keep the flight-energy record
Record route, distances, speed, stop count, state times, state currents, payload, wind, temperature, pack health, reserve, result, owner, and retest trigger.
7. Check yourself
Why is the naive result 4.83%?
Why are there 102 equivalent seconds?
Does 5.67% prove the mission is safe?
The worked values are traceable chapter examples or explicitly labelled teaching assumptions.
- 37 s and 50 s
- Explicit chapter mission times
- 1.3×
- Catalog-typical teaching ratio
- 5.67%
- Two-state energy estimate
Correct, not complete: field evidence still decides acceptance.
Motion Marley guides