A06_Specs.pdf

SPECIFICATIONS

1. Product Features

Name of Item: High-Resolution Airborne Photogrammetric Camera System

Manufacturer: Phase One, Trimble Applanix, or approved equal

Reference Components / Model Numbers:

Part Number Reference Component

73298000 Phase One iXM-GS120 camera body QTY 2 73209000 Rodenstock RS 150 mm aerial lens QTY 2 73328000 Phase One iX Controller MK6, including AP+ interface and minimum 8 TB storage QTY 1 76014700 Trimble Applanix AP+ 18 Air GNSS/Inertial receiver with IMU79 QTY 1 75098510 21-inch operator monitor with keyboard and mouse QTY 1 75098470 AC power supply for iX Controller MK6 QTY 1 75098390 iX Plan software / dongle license, one seat QTY 1 75098370 iX Flight Pro software license QTY 1 70307000 Multi-Sync cable, straight, 1 m QTY 1 70310000 iX camera power cable, straight, 2 m QTY 2

All reference products may be substituted with an approved equal that meets or exceeds the minimum salient characteristics below.

Salient Characteristics:

Camera and Lens (two each)

• Medium-format digital aerial camera with a minimum resolution of 120 megapixels and RGB imaging capability.

• CMOS global-shutter sensor with a minimum image resolution of 12,768 x 9,564 pixels.

• Sensor dimensions of at least 43.9 x 32.9 mm with pixel size no larger than approximately 3.45 micrometers while meeting the required sensor dimensions and resolution.

• Electronic global shutter capable of exposure times of 1/16,000 second or faster to minimize image distortion and motion blur during airborne acquisition.

• Dynamic range of at least 80 dB and RGB sensitivity range that includes ISO 200 through ISO 6400.

• Continuous image acquisition of at least 2 frames per second with image previews.

• 10 Gigabit Ethernet and USB 3.0 or faster interfaces for image transfer and camera communications.

• Removable solid-state internal image storage with a capacity of at least 1 TB.

• Hardware support for external triggering and multi-camera synchronization of 50 microseconds or better.

• Camera body weight not to exceed 0.7 kg (1.55 lb), excluding lens, and body dimensions not to exceed approximately 100 x 100 x 80 mm.

• Operating temperature range shall include at least -10 degrees C to +40 degrees C, with IP53 or better environmental protection.

• FCC Class A, CE, and RoHS compliant, or equivalent applicable certifications.

• Camera and lens shall be suitable for metric photogrammetry and supplied with factory calibration information sufficient for photogrammetric processing and direct georeferencing.

• Fixed 150 mm aerial lens, individually calibrated for infinity focus and high-resolution aerial imaging.

• Lens aperture range shall include at least f/5.6 through f/22.

• Lens - Integrated central/leaf shutter capable of exposure times of 1/2,500 second or faster when mechanical leaf-shutter operation is used.

• Lens/shutter system rated for at least 500,000 shutter actuations.

• When paired with the required camera sensor, nominal field of view shall be approximately 16.7 degrees along the long sensor dimension and 12.6 degrees along the short sensor dimension, or provide equivalent or greater ground coverage at a nominal 150 mm focal length.

• Lens construction shall be suitable for airborne vibration and shock environments and maintain optical and geometric stability during aerial acquisition.

Camera Controller - iX Controller MK6 or Approved Equal

• Rugged airborne camera controller capable of controlling, powering, communicating with, and synchronizing at least four aerial cameras.

• Capable of interfacing with a compatible gyro-stabilized camera mount.

• Integrated support for an onboard survey-grade Applanix AP+ GNSS/Inertial receiver or approved equal.

• Processor performance equivalent to or greater than an Intel Xeon E-class processor and a minimum of 64

GB RAM.

• Minimum of four USB 3.0 ports dedicated to camera communications, plus additional peripheral communications capability.

• Minimum of three Ethernet ports and display outputs adequate to support pilot/operator displays.

• Dedicated secured power connections for at least four cameras and connected peripherals.

• Controller input power compatible with 24-30 VDC aircraft power.

• Minimum 8 TB removable solid-state image/data storage.

• Active cooling and rugged metal construction suitable for aircraft vibration and continuous airborne operation.

• Operating temperature range shall include at least -10 degrees C to +40 degrees C.

• System shall support synchronized image capture, image storage, camera control, GNSS/IMU integration, and metadata/geotag generation within one integrated acquisition system.

GNSS/Inertial Navigation System - AP+ 18 Air with IMU79 or Approved Equal

• High-performance, survey-grade, multi-frequency GNSS/Inertial navigation receiver designed for airborne mapping and direct georeferencing.

• Integrated onboard IMU with solid-state inertial sensors equivalent to Trimble Applanix IMU79 performance or better.

• GNSS tracking shall include, at minimum, GPS L1/L2/L5 and support for multiple major constellations including GPS, GLONASS, Galileo, and BeiDou.

• Support for dual GNSS antennas and GNSS-based heading aiding.

• Real-time position and attitude output rate of at least 100 Hz.

• Raw IMU data logging rate of at least 200 Hz and raw GNSS data logging rate of at least 5 Hz.

• Logging of time tag, status, position, attitude, velocity, track and speed, dynamics, performance metrics, raw IMU data, and raw GNSS observations for post-processing.

• Event input/time-mark capability for precise synchronization of camera exposure events with GNSS/INS data.

• Support for in-air alignment and GNSS-aided inertial navigation.

• Compatible with Applanix POSPac MMS or equivalent post-processing software for direct georeferencing.

• Post-processed absolute RMS accuracy shall be 0.020 m horizontal position or better, 0.050 m vertical position or better, 0.015 m/s velocity or better, 0.025 degrees roll/pitch or better, and 0.080 degrees true heading or better under appropriate processing and operating conditions.

Flight Management and Camera Control Software - iX Flight Pro or Approved Equal

• Fully integrated with the supplied camera, camera controller, GNSS/IMU system, and supported stabilized camera mount.

• Imports and executes flight plans generated by the required flight-planning software.

• Automatically triggers the camera or camera array at planned image-capture locations and records corresponding exposure events.

• Provides real-time system status and camera/acquisition information to the system operator.

• Provides pilot navigation guidance showing planned flight lines, aircraft position and trajectory, cross-track/localizer information, and required flight altitude.

• Provides real-time image preview/review during acquisition and graphical indication of completed and missed image coverage.

• Allows the operator to manage flight-line sequence and start/stop image collection during flight.

• Provides in-flight reflight/replan capability for missed or unacceptable acquisition areas.

• Provides pre-flight system checks and a simulation or equivalent test/training mode.

• Provides post-flight collection reporting that identifies captured and missed images and evaluates collection performance against mission requirements such as overlap, sidelap, altitude, and aircraft trajectory.

Flight Planning Software - iX Plan or Approved Equal

• Photogrammetric aerial mission-planning software with predefined parameters for the proposed camera, lens, and aerial system.

• Allows definition/import of project area, camera/lens configuration, ground sample distance (GSD), forward overlap, side overlap, flight altitude, digital terrain/elevation data, base maps, and ground control points.

• Automatically calculates and generates flight lines and image trigger locations based on sensor parameters, project parameters, terrain height, GSD, and overlap requirements.

• Supports digital terrain models (DTM/DEM) for terrain-aware flight planning.

• Provides graphical visualization and quality assurance of planned GSD, coverage, and image overlap throughout the project.

• Allows flight-line editing and placement/presentation of ground control points.

• Exports flight plans in a format directly usable by the required flight-management/camera-control software.

• Generates project analysis and planning reports sufficient to document acquisition parameters and support project cost/flight-time estimation.

• License shall include a minimum of one planning-software seat and required hardware dongle or equivalent license mechanism.

Operator Monitor

• Dedicated operator display with a minimum screen size of 21 inches.

• Compatible with the supplied iX Controller MK6 or approved equal and capable of displaying the flight-management/camera-control software, image previews, navigation information, system status, and acquisition quality-control information.

• Includes all required display and power connections for normal system operation.

AC Power Supply and System Cabling

• AC power supply for the camera controller, Phase One P/N 75098470 or approved equal, suitable for powering the controller during system setup, testing, data download, and other operation when aircraft

DC power is not used.

• Multi-camera synchronization cable, straight approximately 1 m, Phase One P/N 70307000 or approved equal.

• Camera power cable, straight approximately 2 m, Phase One P/N 70310000 or approved equal.

• All cables shall use secure connectors appropriate for an aircraft vibration environment.

• The contractor shall provide all additional camera, synchronization, GNSS antenna, Ethernet/data, display, power, and peripheral cables required to deliver a complete and operational system.

Integrated System Capabilities

• All camera, lens, controller, GNSS/IMU, operator-display, flight-control software, and flight-planning software components shall be fully integrated and mutually compatible.

• The system shall provide synchronized image capture and GNSS/INS event recording sufficient to associate each image with position, altitude, roll, pitch, and heading information for photogrammetric processing and direct georeferencing.

• The camera/controller system shall be capable of integration with commercially available airborne flight-management systems and compatible stabilized mounts.

• The contractor shall provide all connectors, adapters, licenses, dongles, storage media, power interfaces, and accessories necessary for a complete, functional system whether or not each accessory is individually identified above.

• Equipment shall be delivered with manufacturer documentation and current software/firmware required for normal operation.

2. Delivery

Prices quoted must be FOB Destination

“F.o.b. destination” means --Free of expense to the Government delivered, on board the carrier’s conveyance, at a specified delivery point where the consignee’s facility (plant, warehouse, store, lot, or other location to which shipment can be made) is located; and

Supplies shall be delivered to the destination consignee’s wharf (if destination is a port city and supplies are for export), warehouse unloading platform, or receiving dock, at the expense of the contractor. The Government shall not be liable for any delivery, storage, demurrage, accessorial, or other charges involved before the actual delivery (or “constructive placement” as defined in carrier tariffs) of the supplies to the destination, unless such charges are caused by an act or order of the Government acting in its contractual capacity. If rail carrier is used, supplies shall be delivered to the specified unloading platform of the consignee. If motor carrier (including “piggyback”) is used, supplies shall be delivered to truck tailgate at the unloading platform of the consignee, except when the supplies delivered meet the requirements of Item 568 of the National Motor Freight Classification for “heavy or bulky freight.” When supplies meeting the requirements of the referenced Item 568 are delivered, unloading (including movement to the tailgate) shall be performed by the consignee, with assistance from the truck driver, if requested. If the contractor uses rail carrier or freight forwarder for less than carload shipments, the contractor shall ensure that the carrier will furnish tailgate delivery when required, if transfer to truck is required to complete delivery to consignee.

Contractor responsibilities. The contractor shall -- (1)(i) Pack and mark the shipment to comply with contract specifications; or

(ii) In the absence of specifications, prepare the shipment in conformance with carrier requirements;

(2) Prepare and distribute commercial bills of lading;

(3) Deliver the shipment in good order and condition to the point of delivery specified in the contract;

(4) Be responsible for any loss of and/or damage to the goods occurring before receipt of the shipment by the consignee at the delivery point specified in the contract;

(5) Furnish a delivery schedule and designate the mode of delivering carrier; and

(6) Pay and bear all charges to the specified point of delivery.

3. Delivery Location:

Product shall be delivered to the following location:

Kenai National Wildlife Refuge

33398 B Ski Hill Rd.

Soldotna, AK

99669

4. Delivery Instructions: NA

No later than three days prior to delivery, please contact the Point of Contact listed above, to notify recipient of shipment.