ADCS 3D SIMULATOR
Quaternion Dynamics · Wheels · Thrusters · Sensors · Antenna · Sun-Tracking Arrays
OFF MODE: OFF STOWED 1.0×
Yaw ψ
0.00°
Pitch θ
0.00°
Roll φ
0.00°
|ω| °/s
0.000
Err°
0.00
q0
1.000
q1
0.000
q2
0.000
q3
0.000
Sim Time
00:00:00
Control Panel
Simulation Time
Speed
1×
0.1× 10×
Presets:
Configuration
Solar Arrays
Mode FIXED
Power —
Array angle Fixed (0°)
Track rate 0.5 °/s max
ConfigStowed
Izz5.0 kg·m²
Ixx/Iyy/Izz5.0/5.0/5.0
Summary5.0/5.0/5.0 kg·m²
Deployable Antenna
StateStowed
Boom length0 / 60 cm
ΔIyy+0.0 kg·m²
Pointing err—
Actuator Config
Control Mode
Target Attitude
Yaw ψ0.0°
Pitch θ0.0°
Roll φ0.0°
PIID Control Gains
Kp
Ki₁
Ki₂
Kd
Disturbance Torques
SRP/GG amp0.00
Thruster bias0.00
Wheel/Satellite Mass Ratio
m_wheel2.0 kg
Iw = ½mR²0.0225 kg·m²
Iw/Isat0.45%
Max H/wheel— Nms
Scenario Presets
Initial Conditions (YPR°, ω°/s)
ψ₀ Yaw
θ₀ Pitch
φ₀ Roll
ωx₀ °/s
ωy₀ °/s
ωz₀ °/s
Satellite View
Sensor Suite
📷 Star Tracker—
🌍 Earth Sensor—
☀️ Sun ±X/±Z—
📡 IMUACTIVE
FOV range (m)1.0
STR FOV (°)10°
Earth Sensor FOV (°)40°
Sun Sensor FOV (°)60°
Attitude Mosaic — 2×2 ⬜ perspective · top · front · side
PERSPECTIVE — 3D
drag orbit · scroll zoom
TOP — +Z DOWN
⊡ reset
FRONT — +X
⊡ reset
SIDE — +Y
⊡ reset
Telemetry
Attitude State
q₀
1.000
q₁
0.000
q₂
0.000
q₃
0.000
Yaw ψ0.00°
Pitch θ0.00°
Roll φ0.00°
ωx0.000 °/s
ωy0.000 °/s
ωz0.000 °/s
Att Error0.00°
|H| total0.000 Nms
📡 AntennaStowed
🔆 SA Power—%
☀️ SA Angle L/R—
PIID Breakdown (Nm)
τP0.000
τI₁0.000
τI₂0.000
τD0.000
τ_dist0.000
Reaction Wheels
RW+X
0 RPM
0.000 Nms
RW+Y
0 RPM
0.000 Nms
RW+Z
0 RPM
0.000 Nms
RW⊕
0 RPM
0.000 Nms
Celestial Bodies (3D Position)
🌍 Earth brg—
☀️ Sun brg—
🌙 Moon brg—
τ_GG (Earth)0.000 Nm
τ_SRP (Sun)0.000 Nm
τ_tidal (Moon)0.000 Nm
Drag bodies in 3D view (right-click drag to orbit)
Angle vs Time
— Actual - - Commanded — Error
Inertia Measurement
Ixx— kg·m²
Iyy— kg·m²
Izz— kg·m²
Event Log