Positioning_System_TRD.docx
DOCX document 48 KB Posted
- Attached to
- Stabilized Positioning System Federal contract opportunity
- Solicitation number
- FA2823-17-Q-0073
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| File | Type | Posted |
|---|---|---|
| Sources_Sought_Gyro_Stabilized_Positioning_System.pdf |
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DEPARTMENT OF THE AIR FORCE
HEADQUARTERS 96TH TEST WING (AFMC)
EGLIN AIR FORCE BASE FLORIDA
SUBJECT: Government Technical Requirement Document: Gyro-Stabilized Positioning System
1. Requirement for a Commercial-Off-The-Shelf (COTS) stabilized positioning system to be used as an instrumentation platform to track airborne targets from a mobile ground location. The platform must meet the following technical requirements.
System
0. 2-axis, elevation over azimuth platform
0. Line-of-sight stabilization
0. Position Resolution: 3 µradians
0. Position Accuracy: +/- 100 µradians
0. Payload up to 150 lbs.
0. Azimuth Travel: +/- 175°
0. Elevation Travel: -15° to +95°
0. Speed: up to 90°/sec
0. Acceleration: up to 90°/sec2
0. Stow locks for travel
0. Operating Temperature: -30°C to +55°C
Mechanical
a. Yoke-style configuration
b. Payload mounting surface: at least 16” perpendicular to line-of-sight x 8” along line-of-sight
c. Positioner Weight ≤ 90 lbs.
Electrical
a. Control Interface: RS-232/422 or Ethernet, ICD or SDK provided
b. Power: 115 VAC, 60 Hz
Control Interface
a. Provide system status updates (Azimuth, Elevation, Rates at minimum) available at a minimum of 30Hz
b. Accept system status updates of at least 30Hz image1.jpeg image10.jpeg
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