The Visual Navigation System (VNS01) provides accurate and resilient navigation to ensure mission success when GNSS signals are unavailable, unreliable, or compromised. Designed for NATO Category I and II Unmanned Aerial Systems (UAS), VNS01 enables assured autonomy in contested and hostile environments.
Combining Visual Odometry (VO), Pattern Recognition (PR), Template Matching, Satellite Map Matching and Terrain Referenced Navigation (TRN), the VNS01 extends GNSS-denied navigation capabilities beyond previously explored areas. In previously mapped terrain, Template Matching provides zero-drift navigation through continuous correlation with referenced imagery. In unknown terrain, preloaded satellite imagery and digital elevation models (DEMs) enable absolute position corrections through Satellite Map Matching and TRN. By continuously fusing data from onboard sensors, the VNS01 provides the Flight Control Computer (FCC) with reliable and accurate positioning information when GNSS signals are unavailable or degraded.
The Visual Navigation System delivers resilient navigation in GNSS-denied environments, supporting assured autonomy in contested operations. Successfully used in real operations under jamming, spoofing and other GNSS-disruption scenarios, it combines Visual Odometry, Satellite Map Matching, Terrain Referenced Navigation and Template Matching to maintain a reliable navigation solution and help ensure mission continuity when conventional navigational sources are degraded or unavailable.
The VNS01 uses Visual Odometry (VO) and onboard sensor fusion to maintain reliable navigation when GNSS signals are unavailable or compromised. By continuously tracking visual features and aircraft motion, it enables dead-reckoning navigation in unknown flight areas without prior reference data, significantly reducing inertial drift and extending the distance and duration over which an effective navigation solution can be maintained.
Terrain Referenced Navigation (TRN) is used by the VNS01 to estimate the aircraft’s absolute position by correlating a sequence of onboard terrain measurements with preloaded Digital Elevation Models (DEM). By considering the terrain profile observed along the flight path (not just individual measurements), the system can identify the aircraft’s most likely position and provide absolute corrections to the inertial navigation solution. This keeps position drift bounded and supports reliable operations in GNSS-denied environments.
Satellite Map Matching allows the VNS01 to transform preloaded satellite imagery into navigation references. By correlating imagery captured by the onboard camera with features from preloaded satellite maps, it continuously performs absolute position corrections, constraining inertial drift and enabling high-precision navigation in GNSS-denied environments.
Due to its small size and weight, the VNS01 can be installed in small and medium-sized UAS, enabling them to benefit from this groundbreaking system without sacrificing autonomy or payload capacity. The compact and lightweight device, specifically designed for NATO Category I and II UAS, is provided as an optional peripheral to the main Flight Control System.
Reduced dimensions, lightweight, and integrated design enable easy installation in unmanned aerial platforms. No complex electrical installations are required due to its simple wiring. Low battery consumption optimizes performance. This makes it suitable for platforms with different sizes, performance requirements and mission profiles.
Operations that require all or part of a mission to be conducted without access to GNSS data are becoming increasingly common. In certain situations, the GNSS signal might encounter disruptions, or the mission may require that the flight be initiated without a GNSS signal from the onset.

UAV Navigation-Grupo Oesía's Flight Control Solutions are designed from the ground up to operate in GNSS-denied environments. While the flight control system can safely maintain aircraft control and navigate in dead-reckoning mode during GNSS outages, prolonged operations without external position updates inevitably lead to accumulated navigation drift. This is where the Visual Navigation System (VNS01) provides a critical advantage, delivering absolute position corrections that constrain drift and maintain precise navigation when GNSS signals are unavailable, unreliable or compromised.
When integrated with the VECTOR flight control systems, the VNS01 reduces inertial drift and delivers more accurate positioning than the MEMS-based inertial navigation systems typically used on this class of aircraft due to size, weight, and power constraints.

The VNS01 processes data from its onboard camera and other sensors to estimate motion and absolute position relative to the environment below, reducing inertial drift over extended periods. In previously surveyed areas, the system can use imagery collected from previous flights as a navigation reference, applying pattern recognition to continuously correct positioning errors and reduce the drift to near-zero levels. In areas that were previously not flown, it can rely on preloaded satellite imagery correlating features captured by the onboard camera. It can also rely on preloaded satellite imagery correlating features captured by the onboard camera.
In addition, the VNS01 employs Visual Odometry (VO) and onboard sensor fusion to maintain reliable dead-reckoning navigation. By continuously tracking visual features and aircraft motion, the system maintains accurate relative positioning even in areas where no prior references are available. Terrain Referenced Navigation (TRN) provides an additional source of absolute positioning by correlating onboard terrain measurements with Digital Elevation Models (DEMs). Together, these capabilities continuously generate position corrections, keeping inertial navigation drift bounded and supporting long-endurance operations in contested GNSS-denied environments.

Through this combination of Visual Odometry, Pattern Recognition, preloaded Satellite Map Matching and Terrain Referenced Navigation, the system enables precise position updates both in known and unknown flight areas. Corrections generated by these algorithms are fused within the navigation estimator, allowing the Flight Control System to maintain bounded and stable navigation performance during prolonged GNSS outages.
This innovative capability is likely to attract attention from manufacturers and end-users of NATO Category I and II UAS, small and medium‑sized UAS. The compact and lightweight device, offered as an optional peripheral to the main Flight Control System (FCS), facilitates the safe and efficient navigation of Uncrewed Aerial Vehicles (UAVs) in GNSS-denied environments.
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TYPICAL DEAD-RECKONING DRIFT FIGURES
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VECTOR autopilot without Visual Navigation System
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4% of distance traveled
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VECTOR autopilot with Visual Navigation System at Known Terrain
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No Drift
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VECTOR autopilot with Visual Navigation System at Unknown Terrain
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Drift constrained to up to 30 meters.
Drift remains bounded and is not cumulative.
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MECHANICAL / ENVIRONMENTAL
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Size (mm, H x W x L)
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22x46x77
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Weight
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100 gr
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Enclosure Material
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Grade 6082 Aluminium Alloy
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IP Rating
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Designed to conform with IP67
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Humidity
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Up to 90% RH, non-condensing
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Internal Memory
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5 GB
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Temperature Range
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-20ºC to +85ºC
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Mounting Screws
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4 x M2.5
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ELECTRICAL
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Supply (unregulated)
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9V to 36V DC
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Power Consumption
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5 W @ 12VDC
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I/O
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CAN 2.0 B
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1 (up to 1Mbps)
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Serial Comm
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1 x RS-232 (up to 250kbps)
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Ethernet
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100 Base Tx Channel according to IEEE 802.3 standard
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The VNS01 Kit includes the connector and wiring needed to connect the Visual Navigation System to the VECTOR family. The kit includes the following:
Operations that require all or part of a mission to be conducted without access to GNSS data are becoming increasingly common. In certain situations, the GNSS signal might encounter disruptions, or the mission may require that the flight be initiated without a GNSS signal from the onset.

UAV Navigation-Grupo Oesía's Flight Control Solutions are designed from the ground up to operate in GNSS-denied environments. While the flight control system can safely maintain aircraft control and navigate in dead-reckoning mode during GNSS outages, prolonged operations without external position updates inevitably lead to accumulated navigation drift. This is where the Visual Navigation System (VNS01) provides a critical advantage, delivering absolute position corrections that constrain drift and maintain precise navigation when GNSS signals are unavailable, unreliable or compromised.
When integrated with the VECTOR flight control systems, the VNS01 reduces inertial drift and delivers more accurate positioning than the MEMS-based inertial navigation systems typically used on this class of aircraft due to size, weight, and power constraints.
The VNS01 processes data from its onboard camera and other sensors to estimate motion and absolute position relative to the environment below, reducing inertial drift over extended periods. In previously surveyed areas, the system can use imagery collected from previous flights as a navigation reference, applying pattern recognition to continuously correct positioning errors and reduce the drift to near-zero levels. In areas that were previously not flown, it can rely on preloaded satellite imagery correlating features captured by the onboard camera. It can also rely on preloaded satellite imagery correlating features captured by the onboard camera.
In addition, the VNS01 employs Visual Odometry (VO) and onboard sensor fusion to maintain reliable dead-reckoning navigation. By continuously tracking visual features and aircraft motion, the system maintains accurate relative positioning even in areas where no prior references are available. Terrain Referenced Navigation (TRN) provides an additional source of absolute positioning by correlating onboard terrain measurements with Digital Elevation Models (DEMs). Together, these capabilities continuously generate position corrections, keeping inertial navigation drift bounded and supporting long-endurance operations in contested GNSS-denied environments.
Through this combination of Visual Odometry, Pattern Recognition, preloaded Satellite Map Matching and Terrain Referenced Navigation, the system enables precise position updates both in known and unknown flight areas. Corrections generated by these algorithms are fused within the navigation estimator, allowing the Flight Control System to maintain bounded and stable navigation performance during prolonged GNSS outages.
This innovative capability is likely to attract attention from manufacturers and end-users of NATO Category I and II UAS, small and medium‑sized UAS. The compact and lightweight device, offered as an optional peripheral to the main Flight Control System (FCS), facilitates the safe and efficient navigation of Uncrewed Aerial Vehicles (UAVs) in GNSS-denied environments.
Map matching at work:



|
TYPICAL DEAD-RECKONING DRIFT FIGURES
|
|
|
VECTOR autopilot without Visual Navigation System
|
4% of distance traveled
|
|
VECTOR autopilot with Visual Navigation System at Known Terrain
|
No Drift
|
|
VECTOR autopilot with Visual Navigation System at Unknown Terrain
|
Drift constrained to up to 30 meters.
Drift remains bounded and is not cumulative.
|
|
MECHANICAL / ENVIRONMENTAL
|
|
|
Size (mm, H x W x L)
|
22x46x77
|
|
Weight
|
100 gr
|
|
Enclosure Material
|
Grade 6082 Aluminium Alloy
|
|
IP Rating
|
Designed to conform with IP67
|
|
Humidity
|
Up to 90% RH, non-condensing
|
|
Internal Memory
|
5 GB
|
|
Temperature Range
|
-20ºC to +85ºC
|
|
Mounting Screws
|
4 x M2.5
|
|
ELECTRICAL
|
|
|
Supply (unregulated)
|
9V to 36V DC
|
|
Power Consumption
|
5 W @ 12VDC
|
|
I/O
|
|
|
CAN 2.0 B
|
1 (up to 1Mbps)
|
|
Serial Comm
|
1 x RS-232 (up to 250kbps)
|
|
Ethernet
|
100 Base Tx Channel according to IEEE 802.3 standard
|
The VNS01 Kit includes the connector and wiring needed to connect the Visual Navigation System to the VECTOR family. The kit includes the following:
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