Gridbots Falcon is a precision gyro stabilised optical platform that holds a mounted sensor on target while the host vehicle pitches, rolls, vibrates and turns. Inertial rate sensing, direct-drive torque motors and a closed-loop servo running at high bandwidth cancel base motion before it ever reaches the optical line of sight.
The Falcon family spans four frame sizes. The compact F1 holds line of sight to 50 µrad RMS with payloads up to 1 kg; the heavy-lift F10 carries up to 10 kg of sensor mass and holds 150 µrad RMS. Every model shares the same servo core, command protocol and mechanical interface, so a payload developed on one frame moves to another without software change.
Falcon accepts any combination of day camera, cooled or uncooled thermal imager, laser range finder, laser designator, spotter scope or SWIR module inside its payload envelope. It ships as an open stabilised gimbal for integrators, or pre-populated with a Gridbots sensor suite for turnkey surveillance, naval observation, airborne survey and vehicle-mounted sighting roles.
Gyro Stabilised Optical Platform
50 to 150 µrad RMS
Line-of-Sight Stabilisation
FOG + MEMS Inertial Sensing
Rate Feedback
1 kg to 10 kg Payload
Four Frame Sizes
Land · Naval · Airborne
Common Servo Core
Four frames, one servo architecture. Stabilisation accuracy trades against carried mass: the lighter the payload and the smaller the inertia, the tighter the loop holds. Pick the frame by payload mass first, then confirm the stabilisation figure meets the mission's angular budget.
| Parameter | Falcon F1 | Falcon F3 | Falcon F5 | Falcon F10 |
| Maximum Payload | 1 kg | 3 kg | 5 kg | 10 kg |
| Stabilisation (RMS) | 50 µrad | 75 µrad | 110 µrad | 150 µrad |
| Stabilisation Axes | 4 (2 coarse + 2 fine) | 4 (2 coarse + 2 fine) | 4 (2 coarse + 2 fine) | 4 (2 coarse + 2 fine) |
| Inertial Sensing | Fibre-optic gyro | Fibre-optic gyro | FOG + MEMS hybrid | FOG + MEMS hybrid |
| Servo Bandwidth | 90 Hz | 70 Hz | 50 Hz | 35 Hz |
| Maximum Slew Rate | 120°/s | 90°/s | 60°/s | 40°/s |
| Angular Acceleration | 250°/s² | 180°/s² | 120°/s² | 80°/s² |
| Pointing Repeatability | 0.2 mrad | 0.3 mrad | 0.4 mrad | 0.5 mrad |
| Azimuth Travel | Continuous 360° | Continuous 360° | Continuous 360° | Continuous 360° |
| Elevation Travel | −60° to +90° | −60° to +90° | −45° to +85° | −40° to +80° |
| Platform Mass (unloaded) | 3.5 kg | 7.5 kg | 13 kg | 24 kg |
| Power (nominal / peak) | 45 / 90 W | 70 / 140 W | 110 / 220 W | 180 / 360 W |
| Ingress Protection | IP66 | IP66 | IP67 | IP67 |
Stabilisation figures are RMS residual line-of-sight error measured at maximum rated payload on a 6-DOF motion table under the reference sea-state / cross-country profile. Lighter payloads improve the figure.
Four-axis stabilisation - coarse gimbal plus fine steering stage
50 µrad RMS line of sight on the F1 frame
Payload capacity from 1 kg to 10 kg across four frames
Direct-drive brushless torque motors - no backlash, no gear train
Continuous 360° azimuth on slip ring
Open payload bay - any EO, IR, SWIR, LRF or designator combination
Common command protocol across the whole model range
Geo-pointing, slew-to-cue and scan patterns built in
Auto payload balancing and inertia auto-tune on power-up
Sealed to IP66 / IP67 with dry-nitrogen purge port
Residual line-of-sight error is what decides whether a long-focal-length sensor produces a usable image from a moving platform. At 50 µrad, the Falcon F1 holds a target inside a single detector pixel of a 90× zoom camera at 2 km. The tables and charts below show measured residual error against base-motion severity and payload mass.
| Base Motion Condition | F1 (1 kg) | F3 (3 kg) | F5 (5 kg) | F10 (10 kg) |
| Static tripod / fixed mast | 18 µrad | 26 µrad | 38 µrad | 52 µrad |
| Metalled road, 40 km/h | 30 µrad | 44 µrad | 62 µrad | 85 µrad |
| Cross-country, 20 km/h | 50 µrad | 75 µrad | 110 µrad | 150 µrad |
| Sea State 3 (naval mast) | 42 µrad | 64 µrad | 95 µrad | 132 µrad |
| Sea State 5 (naval mast) | 65 µrad | 98 µrad | 140 µrad | 195 µrad |
| Rotary-wing airframe vibration | 55 µrad | 82 µrad | 125 µrad | — |
Values are RMS residual line-of-sight error at maximum rated payload for each frame. Quoted headline accuracy corresponds to the cross-country reference profile.
Logarithmic scale. An unstabilised hard mount passes base motion straight to the optical axis; the Falcon servo rejects it by two to three orders of magnitude.
The payload bay is an open mechanical volume with a bolt pattern, power rails and data lanes brought through the slip ring. Mount a sensor, declare its mass and centre of gravity, and the platform runs an inertia auto-tune on the next power-up. No servo re-tuning by hand, and no controller firmware change when moving a payload between frames.
| Payload Bay | F1 | F3 | F5 | F10 |
| Rated Mass | 1 kg | 3 kg | 5 kg | 10 kg |
| Usable Volume (L×W×H) | 180×140×120 mm | 260×190×170 mm | 340×240×220 mm | 460×320×290 mm |
| CG Offset Tolerance | ±8 mm | ±12 mm | ±18 mm | ±25 mm |
| Payload Power Available | 40 W | 80 W | 150 W | 300 W |
| Data Lanes Through Slip Ring | 2× GigE, 1× RS-422 | 2× GigE, 2× RS-422 | 4× GigE, 2× RS-422 | 4× GigE + CoaXPress, 4× RS-422 |
| Typical Payload | Mass | Recommended Frame |
| HD day camera, 30× zoom | 0.6 - 0.9 kg | Falcon F1 |
| Uncooled LWIR imager (640×480) | 0.4 - 0.8 kg | Falcon F1 |
| Day camera + uncooled thermal + LRF | 2.2 - 2.8 kg | Falcon F3 |
| Cooled MWIR imager with continuous zoom | 3.5 - 4.5 kg | Falcon F5 |
| Long-range EO/IR suite + eye-safe LRF + SWIR | 4.5 - 5.0 kg | Falcon F5 |
| Multi-sensor suite with large-aperture telescope | 7 - 10 kg | Falcon F10 |
| Survey / mapping camera with IMU-INS block | 6 - 9 kg | Falcon F10 |
| Model Number | GB-FALCON (F1 / F3 / F5 / F10) |
| Type | Gyro Stabilised Optical Platform / 4-Axis Stabilised Gimbal |
| Line-of-Sight Stabilisation | 50 µrad RMS (F1) to 150 µrad RMS (F10) |
| Payload Capacity | 1 kg (F1), 3 kg (F3), 5 kg (F5), 10 kg (F10) |
| Stabilisation Architecture | Two-axis coarse gimbal with two-axis fine steering stage |
| Inertial Sensing | Fibre-optic rate gyro; FOG + MEMS hybrid on F5 / F10 |
| Drive | Direct-drive brushless torque motors, gearless |
| Angle Feedback | Absolute optical encoder, 22-bit |
| Azimuth Travel | Continuous 360° (slip ring) |
| Elevation Travel | −60° to +90° (frame dependent) |
| Slew Rate | 40°/s to 120°/s (frame dependent) |
| Pointing Repeatability | 0.2 mrad to 0.5 mrad |
| Modes | Stabilised stare / Manual / Geo-point / Scan / Slew-to-cue / Track follow |
| Navigation | Differential GPS, dual-channel compass, 10-DOF low-drift IMU |
| Interface | Gigabit Ethernet, RS-422, CoaXPress (F10), discrete I/O |
| Control Protocol | Gridbots open gimbal protocol; common across all frames |
| Input Power | 18 - 32 VDC; 45 W to 180 W nominal by frame |
| Ingress Protection | IP66 (F1 / F3), IP67 (F5 / F10) |
| Operating Temperature | −30 °C to +60 °C |
| Environmental | Designed to MIL-STD-810; EMI/EMC to MIL-STD-461 |
| Mounting | Vehicle roof, telescopic mast, naval deck pedestal, airborne nose ball |




The Gridbots Falcon is a four-axis gyro stabilised optical platform built for sensors that have to stay on target from a moving host. As a stabilised gimbal it uses direct-drive torque motors, absolute encoders and fibre-optic rate gyros to reject base motion, delivering line-of-sight stabilisation from 50 µrad RMS on the compact F1 frame through to 150 µrad RMS on the heavy-lift F10. Payload capacity spans 1 kg to 10 kg, so the same platform family covers a single lightweight day camera on a UAV, a fused EO/IR and laser range finder suite on a vehicle mast, and a large-aperture long-range telescope on a coastal or naval pedestal. Continuous 360° azimuth, geo-pointing, slew-to-cue and a shared control protocol across every frame make the Falcon a straightforward stabilised camera platform for integrators building surveillance, observation, survey and sighting systems.