Vision Aided Navigation (VAN) navigation system
Also known as: VisionAidedNavigation(VAN), Vision-Aided-Navigation-(VAN), Honeywell Aerospace Vision Aided Navigation (VAN), Honeywell Aerospace VisionAidedNavigation(VAN)
Vision Aided Navigation (VAN) is a navigation system that uses environmental observations to support vehicle positioning. It provides navigation information for an integrated autonomy system, complementing the aircraft guidance and control functions.
Description
Vision Aided Navigation (VAN) is a visual navigation system from Honeywell Aerospace that gives an aircraft an absolute position fix without GNSS. It belongs to Honeywell's alternative navigation family and works by image correlation: a live camera feed, optical or infrared, is compared with reference maps carried on board, and the match produces the position of the vehicle. It is meant for GNSS-denied and GNSS-disrupted operation of large unmanned aircraft, military aircraft and other platforms that need a backup to satellite navigation.
Because the position comes from matching the scene to a map, the error does not grow with time as it does in an inertial system running alone. Honeywell describes the result as a true absolute position fix that does not drift, and it reports a demonstrated horizontal position accuracy below 10 m CEP50 during GPS-denied conditions, shown on an Embraer E170 test aircraft. For an integrator this means VAN is used to bound inertial drift during a long GNSS outage, not to replace the inertial navigation system.
The method is passive, so it emits no signal that can be jammed, spoofed or detected. It is sensor agnostic, with cross-modal correlation, which allows visible and infrared sensors to be used and permits day and night operation. It is also stated to be robust to changes in lighting and season and to map staleness, and it has low map storage requirements, so a large area can be stored without building a mission-specific database for each flight. The prior map is a requirement of the method.
For integration, the hardware demonstration unit measures 14 x 21 x 25 cm, weighs 13 lb, and draws up to 34 W from a 28 V DC input, with an operating temperature range of -40 to 70 degrees C. Inputs are 28 V DC and an altitude measurement from a pressure or radar altimeter, and the interfaces are Ethernet and MIL-STD-1553. The vibration reference is the random B curve of DO-160E section 8. VAN is compatible with the Honeywell Compact Inertial Navigation System and other inertial platforms, and it is designed to be integrated into Honeywell's Alternative Navigation Architecture, the software layer that combines vision with magnetic, celestial and inertial inputs. It is offered as a software-only solution as well as with hardware options.
Honeywell lists the target applications as GPS-denied or disrupted operations, backup navigation for various aircraft and munitions guidance. Within its layered navigation strategy VAN sits alongside magnetic anomaly aided navigation and celestial navigation, for platforms that must keep navigating where satellite signals are unavailable.
Specifications
| General | |
|---|---|
| Grade | Aerospace-grade |
| Market | Dual-use |
| Platform class | Large UAS (25–150 kg), Heavy UAS (>150 kg), Manned aircraft |
| Airframe | Any |
| Availability | In production |
| Dimensions (L × W × H, mm) | 14x21x25 cm[4] |
| Operating temperature | -40 – 70 °C[4] |
| Key specifications | |
| Navigation method | Landmark matching[1] |
| GNSS-denied operation | Yes[1] |
| Day / night | Day/night capability; sensor selection and reference-map suitability are installation dependent.[1] |
| Additional specifications | |
| Prior map required | Yes[1] |
Sources
- honeywellaerospace.com/us/en/products-and-services/products/navigation-and-sensors/navigation-systems/vision-aided-navigation · checked October 25, 2026
- prod-edam.honeywellaerospace.com/content/dam/honeywell-edam/aero/en-us/products/navigation-and-sensors/navigation-systems/vision-aided-navigation/documents/hon-aero-vision-aided-navigation-brochure-1493615-n61-3150-000-000.pdf · checked October 25, 2026
- prod-edam.honeywellaerospace.com/content/dam/honeywell-edam/aero/en-us/products/navigation-and-sensors/navigation-systems/vision-aided-navigation/documents/hon-aero-honeywell-alternative-navigation-brochure.pdf · checked October 25, 2026
- prod-edam.honeywellaerospace.com/content/dam/honeywell-edam/aero/en-us/products/navigation-and-sensors/navigation-systems/vision-aided-navigation/documents/hon-aero-vision-aided-navigation-brochure-1493615-n61-3150-000-000.pdf · checked November 8, 2026
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Frequently asked questions
How does the Vision Aided Navigation (VAN) system provide positioning?
The system provides navigation by comparing real-time imagery to preloaded reference maps.
Is the VAN system compatible with different types of optical sensors?
Yes, the system is sensor-agnostic and supports various optical sensors, including visible and infrared.
Does the VAN system require mission-specific databases for map storage?
No, the system uses efficient algorithms that allow for large-area coverage without needing mission-specific databases.
Is the VAN system compatible with existing inertial navigation platforms?
The system is compatible with the Honeywell Compact Inertial Navigation System (HCINS) and other inertial platforms.
Is the VAN system vulnerable to GPS jamming or spoofing?
The system is passive and secure, making it immune to jamming, spoofing, or detection.
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