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CG Balancing Tool

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Airframe

Designation

MTOW kg

Empty Wt kg

Fuse Length m

Fuse Dia m

Configuration

STOL

VTOL

HYBRID

TAIL-SITTER

Fuselage Shape

Payload kg

CG % MAC

Landing Gear

Include Landing Gear

Gear Type

TRICYCLE

TAIL-DRAGGER

SKID

FLOAT

Leg Height m

0.22

Track Width m

0.22

Wheel Dia m

Wheelbase m

Position Along Fuselage

0 = nose tip · 1 = tail end
Main gear attaches at X_main, nose/tail wheel at X_nose

Main Gear X ×L

Nose/Tail Wheel X ×L

Vertical Attach Offset m below fuselage CL

Wing Geometry

Wingspan m

Wing Area m²

Wing Configuration

STRAIGHT

TAPERED

DELTA

SWEPT

X-WING

BIPLANE

Taper Ratio

Sweep °

Dihedral °

Incidence °

Airfoil

Series

ID / Code

Thick %c

Camber %c

AoA °

Control Surfaces

Aileron %chord

Aileron %span

Elevator m²

Rudder m²

Tail Type

CONV

T-TAIL

V-TAIL

H-TAIL

X-TAIL

NO-TAIL

Propulsion

Type

ELECTRIC

ICE

HYBRID

TURBOFAN

Motor Power W

Num Motors

Motor Placement

NOSE

PUSHER

WING

MULTI-ROTOR

Prop Dia in

Prop Pitch in

Motor Position (NOSE/PUSHER/WING)

X: 0=nose → 1=tail along fuselage
Y: vertical offset from fuse CL (m, +=up)
Z: lateral offset from CL (m, +=stbd)

X ×L

Y m

Z m

Motor Orientation (tilt angles °)

Tilt X = pitch (nose-up +) · Y = yaw · Z = roll

Tilt X °

Tilt Y °

Tilt Z °

Propeller

Spin Direction

Arm Length m (WING/MR)

Energy Source

Batt Cap mAh

Cell Config

Fuel Vol L

Endurance min

Cruise Speed m/s

Max Speed m/s

Stall Speed m/s

Mission Profile

Mission Type

ISR

MAPPING

DELIVERY

COMMS RELAY

TLH

Range km

Ceiling m

Op Alt m AGL

Max Wind m/s

Launch Method

Recovery Method

Notes

Avionics & Sensors

Flight Controller

Telemetry

Data Rate kbps

Ctrl Range km

Video Link

GNSS

GPS

GPS+GLO

GPS+GAL

FULL

Payload

Primary Sensor

Gimbal

Sensor Wt kg

Storage GB

CG Balancing

Datum = Nose tip · X along fuselage (m from nose) · Y along wing span (m from CL, + = starboard)

Component Mass Table

Quick-Fill from Design

CG Result

CG — X (from nose)

—

— % fuselage length

CG — Y (span)

—

— % half-span

TOTAL MASS

—

vs MTOW

—

ADD COMPONENTS TO CHECK BALANCE

FUSELAGE CG DIAGRAM — SIDE VIEW

WING SPAN CG DIAGRAM — TOP VIEW

✈

NO MODEL LOADEDSet parameters & press GENERATE

▶ X — LONGITUDINAL

▲ Y — VERTICAL

● Z — LATERAL

W/L — kg/m²

AR —

T/W —

CL —

COMPUTING GEOMETRY…

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DESIGNATION

—

WINGSPAN

—

MTOW

—

WING LOAD

—

ASPECT R.

—

CRUISE

—

RANGE

—

ENDURANCE

—

CONFIG

—

PROPULSION

—

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