PGC-A (Autonomous Portable Glass Cockpit)
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PGC-A is an electronic pilot assistant that improves efficiency in normal flights and increases safety in heavy conditions. It supports wide range of missions, from flight training and general aircraft piloting to special missions, search & rescue and surveying. While PGC-A capabilities and functionality are equal or even better than of standard aircraft instruments, it can be also used as a back-up system on any type of airplane or helicopter.
- Flight planning and post-mission analysis
- Flight training and simulation
- Primary flight display (PFD)
- Navigation (ND) and moving map displays
- Standard instruments display
- Combination of displays and screens
- Forward-looking 3D views of terrain and TAWS
- Obstacles and planned flight trajectory indication
- Predictive flight guidance (from take-off to landing)
- Quick charts and digital terrain maps upload
- Wind parameters identification
- Direct-to function
- Store/recall navigation points
- AS/SI measurement systems
- Indicated parameter source switching
- Navigation signal source monitoring
- Approach and landing pattern programming
Provides the functionality of
- EFIS Electronic Flight Instrumentation System
- FMS Flight Management System
- TAWS Terrain Awareness and Warning System
- FD Flight Director
- EFB Electronic Flight Bag
PGC-A is an electronic perspective predictive flight guidance system, which optionally uses synthetic terrain imagery in the background. It was designed as a hardware-software integrated system based on CompaNav-2 inertial navigation system complemented by proprietary “pictorial indication” software.
PGC-A affordably brings advanced piloting and navigation tools (EFIS, Flight Management/ Flight Director systems) even to the cockpits of light airplanes and helicopters. It is a portable system, based on modern computer and microelectronic technology, highly reliable and fast to deploy, that fits into a briefcase and offers a complete solution for navigation, instrument flight and even more.
PGC-A Architecture

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PGC-A Standard Architecture
- CompaNav-2 Inertial Integrated System
- Panasonic CF-18 ruggedized tablet PC
- Garmin GPS35 receiver
- Optional commutation unit
- Flight Data Recorder
- Air Data System (option)
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PGC-A Enhanced Architecture
- CompaNav-2 Inertial Integrated System
- Panasonic CF-18 ruggedized tablet PC
- Garmin GPS35 receiver
- Optional commutation unit
- Flight Data Recorder
- Air Data System (option)
The enhanced architecture of PGC-A offers the interoperability between pilot and co-pilot. Both computers, connected via local network are able to control indication and data base of each other. The backup of inertial and GPS system is provided via commutation unit.
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System Performance
Flight Guidance and Primary Flight Display

By interpreting flight dynamics PGC-A displays flight and navigation data as 3D and 2D graphics using clear images and shapes. In particular, the system can:
- Generate a visual image of a flight in real time and enhances spatial ability of a pilot (especially in heavy flight conditions)
- Provide warnings about possible exceedance of operational limits and ensures terrain collision awareness with the right timing
- Supply a pilot with accurate prompts about aircraft steering in order to maintain the required flight parameters
Moving Map and Digital Terrain
The combined INS and GPS navigation data is displayed on the moving map, providing
- Easy navigation on the moving map and accurate aircraft guidance along the designed trajectory;
- Automatic landing approach programming
- Capability for a low altitude flight, following of the terrain with hills, and for obstacle avoidance using digital pictures of terrain
Flight Planning and Flight Analysis
 Flight Planning |
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PGC-A provides capability for extensive flight planning using known aeronautical databases and digital maps. It supports georeferenced charts in publicly accessible format. Using PGC-A a pilot can create an approach pattern for any landing point taking into consideration local terrain and wind conditions. A virtual flight mode is available for pre-flight training purposes.
Flight Analysis
The flight data stored by Flight Data Recorder (optional unit connected to PGC-A) can be played back to allow flight analysis and identification of the errors made. 3D flight visualisation is available with optional software
Downloads
System overview è system specification
Autonomous Portable Glass Cockpit System
Learn more about PGC-A in the article:
Flying with personal INS (by Dr. Vladimir Voronov , European Journal of Navigation ¹3, 2006)
Video
PGC-A: digital map (16 Mb)
Flight Mi-2 by PGC-A (1,6 Mb)
Flight Mi-8 by PGC-A (5 Mb)
PGC-A: Hovering mode (1,1 Mb)
PGC-A: Landing (1,6 Mb)
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