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Estimating performance factors – ProgressiveRC 4S Gold FMA Cellpro User Manual

Page 8

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Estimating performance factors

If you don’t have a way to directly measure your propulsion system’s electrical parameters, the

Cellpro 4s Charger enables you to estimate them using before- and after-flight measurements.

1. Collect data

a. Charge pack.
b. When charging is finished, record Fuel % and total pack voltage (i.e. sum of cell volt-

ages).

c. Fly plane (or test on the ground). Record flight time in minutes.
d. Connect pack to charger. Record Fuel % and total pack voltage.

2. Calculate performance factors

(Fuel % before flight) – (Fuel % after flight)

100

x (Pack capacity, Ah) =

Capacity consumed during flight, Ah

(Capacity consumed during flight, Ah) x 60

(Flight time, minutes)

=

Average current during flight, A

(Pack voltage before flight, V) + (Pack voltage after flight, V)

2

=

Average voltage during flight, V

(Average voltage during flight, A) x (Average current during flight, V) =

Average power during flight, Watts

The “LiPo Performance Estimator” spreadsheet, which simplifies these calculations, can be

downloaded from www.fmadirect.com/tech_data/techdocs/.

3. Evaluate results

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Average current during flight gives you a rough idea whether system components—ESC,

motor, connectors and wiring—are operating within their current ratings. Keep in mind that

peak current during flight may greatly exceed the average current you calculated.

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Watts per pound is an approximate indicator of aircraft performance (other factors influenc-

ing performance include lift, drag and motor type). Here are some guidelines:

25 to 30 watts per pound: level flight.

40 to 50 watts per pound: take off from smooth surface, climb.

50 to 75 watts per pound: take off from grass, sport aerobatics.

75 to 125 watts per pound: pattern aerobatics.

Over 125 watts per pound: 3D.

Tip: For more direct electrical measurements, consider these FMA products:

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60A Current Shunt (Model DVM-SHUNT-60)

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Digital Multimeter (Model DVM-VC890D)

(Average power during flight, Watts)

(Model weight, pounds)

=

Watts per pound