INTEGRATED DYNAMICS flight control and autopiloting systems employ the latest in micro-electronics and guidance technology. Advanced features and reliable performance are offered in surprisingly powerful and affordable avionics packages. Four models are offered, ranging from simple two-axis electronic stabilization to fully autonomous, GPS-based integrated flight control systems.
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| F L I G H T C O N T R O L S Y S T E M S | ||
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| A P - 2 0 0 0 |
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The AP- 2000 is specially designed for
flight control of low-cost or expendable UAV's and aerial targets.
The AP-2000 system offers superior performance without the
complexity and cost normally associated with full-blown UAV
autopilot systems. The autopilot provides conventional wing
leveling, and height- lock features in a compact package and is easy
to calibrate, with its AUTOTRIM feature, for a variety of airframes. |
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The AP-5000 provides the conventional wing leveling and height lock features of the AP-2000 with the addition of a GPS-based return-home and heading module in a compact package which is easy to calibrate for a variety of airframes not requiring the learning-curve of more complex auto-piloting systems. |
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IFCS-6000 (Integrated Autonomous Flight Control System) |
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The IFCS-6000 provides precise and stable flight control that greatly simplifies UAV flight operaton. By utilizing 'Smart’ electronics, solid-state gyros and inertial sensors, our IFCS- |
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6000 system offers superior performance
without the complexity and cost normally associated with competing
UAV autopilot systems. Total solid-state design significantly
reduces electrical power requirements while increasing reliability
and performance. |
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A variety of airframe types can be accommodated without complicated adjustments and calibration usually required with conventional autopilot systems. The IFCS-6000 accepts command inputs from a laptop PC allowing UAV's to operate autonomously or under remote operator control. Latitude, longitude, speed, heading, altitude, time, date, and waypoint |
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status, as well as video imagery, can all be continuously transmitted via data downlinks to ground control stations . Ground display requirements are minimal and require no more than a simple PC or laptop computer. |
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| Multiple control I/O is supported by allowing sensor data to be displayed using INTEGRATED DYNAMICS unique SENSORVIEW software. | ||
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IFCS-7000 (Integrated Autonomous Flight Control System) |
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The IFCS-7000 is INTEGRATED DYNAMICS next-generation UAV flight control system designed for military users. It incorporates all the features of the IFCS-6000 and provides |
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the added versatility of a 6DOF Inertial Measurement Unit (IMU) and GPS/INS interface. Sensor outputs can be viewed using our SENSORVIEW software. The IFCS-7000 also allows interfacing of payloads and on-board systems into a compact ‘smart’ electronics package and makes the UAV more intelligent by performing demanding tasks without external operator intervention. The IFCS-7000 also provides interface data for controlling our ATPS-1200 and ATPS-2000 Antenna Tracking & Positioning Systems. The IFCS-7000 is a low cost integrated flight control system incorporating navigation, stability, and control. These capabilities include airspeed hold, altitude hold, turn coordination, GPS navigation, autonomous |
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| takeoff and landing (with the LARS-1700 Auto-Land system). Extensive data logging and manual overrides are also supported, as is a highly functional command buffer. All feedback loop gains and flight parameters are user programmable. Expansion options, in the form of several customized modules, are available. A PC based mission simulator is also available for the IFCS-7000. |
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The IFCS-6000 and IFCS-7000 share the following common features: |
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| Completely autonomous operation | ||
| Auto takeoff and land capability* | ||
| 3 microprocessors and dual sensors for increased redundancy** | ||
| On-the-Fly mission changes** | ||
| Includes all sensors required for complete airframe stabilization, control and navigation | ||
| Surface Mount components used for reduced size and increased reliability | ||
| Multiple waypoint GPS navigation linked to INS/IMU** | ||
| Manually piloted, Manually directed and autonomous flight modes | ||
| Supports flaps, flaperons, elevons, v-tail, split rudders, and flap/aileron mixing | ||
| User programmable feedback gains and flight parameters | ||
| Low battery warning both on the ground and in flight | ||
| User programmable error handlers for loss of GPS signal, loss of RC signal, loss of data link,low battery voltage. | ||
| 6 DOF IMU . | ||
| 3 Rate Gyros & 3 accelerometers. | ||
| 2-channel data-logging | ||
| * Supported with expansion module for IFCS-7000 only. | ||
| ** IFCS-7000 only. | ||
| Expansion Module Options: | ||
| - Barometric Altitude Control System (BACS) | ||
| - Barometric Altitude Hold Module (AHS) | ||
| - Engine Management System (EMS) | ||
| - Telecommand interfaces up to C & X Bands | ||
| - Radar Altimeter Module (RAM) | ||
| - Las-er Range-finding Module (LRM) | ||
| - SIGINT Module | ||
| - ELINT Module | ||
| - Payload Control Module (RECON) | ||
| - Communications Repeater Module (COM-R) | ||
| - Communications Jammer Module (COM-J) | ||
| - Dual Power Source Backup Module (DPM) | ||
| - MDI Module – Acoustic Radar | ||
| - Mission Analysis Module (MAM) | ||
| - Flight Data Recorder Module (FDR) | ||
| - Multi-UAV Control Module | ||
| - AHRS module. | ||
| - Night Ops Module (NOPS) | ||
| - Auto Land Module – (LARS-1700 | ||
| - Auto Take off Module | ||
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