SOW.pdf
PDF 563 KB Posted
- Attached to
- Bugeye Control Loader Federal contract opportunity
- Solicitation number
- 80NSSC24875146Q
About this file
The document provided is a Statement of Work (SOW) for a Bugeye Control Loader. The SOW outlines the objectives and requirements for the Bugeye Control Loader, which is designed to support stand-alone operation and electronic synchronization for pilot/co-pilot situations. The device features a reconfigurable grip connector, an integrated I/O card, and Bugeye FFM software that allows users to create customized flight profiles without coding. The period of performance is 90 days after contract award, and the place of performance is the NASA Armstrong Flight Research Center at Edwards Air Force Base.
The related federal contract opportunity is for a sole-source acquisition of the Bugeye Control Loader by the National Aeronautics and Space Administration Shared Services Center (NASA/NSSC). The solicitation number is 80NSSC24875146Q, and the NAICS code is 339999. NASA/NSSC intends to award a sole-source contract to Bugeye Technologies, Inc. under the authority of FAR 13.106-1(b)(1)(i), as Bugeye Technologies, Inc. is the sole provider of the Bugeye Control Loader. The Government intends to acquire commercial items and services using the provisions, clauses, and procedures prescribed in FAR Part 12 and FAR Part 13.
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Text version
Statement of Work (SOW)
1. Objectives and Requirements:
2. Characteristics, Scopes, and Specs:
Supports stand-alone operation as well as electronic synchronization for pilot/co-pilot situations.
Designed to allow for different gear assemblies to be installed into the same mechanism, resulting in higher or lower force outputs at the stick as required.
A reconfigurable grip connector to allows all Bugeye grips to be installed.
An integrated I/O card that converts grip input signals to USB and Ethernet output for the host simulation.
Bugeye FFM Software Included. Software features include:
1. End users can create customized flight profiles for a wide variety of aircraft with no coding required.
2. Does not require its’ own computer. It can be loaded directly on the host computer.
3. Software can be bypassed when the host simulation contains a flight model or force profile within it.
Communication via UDP protocol with the host.
Forces (2-axis) applied to the grip with a minimum update rate of 60 Hz.
Utilizes components that eliminate backlash and mechanical wear resulting in smooth and maintenance free operation.
3. Place of Performance:
Nasa Armstrong Flight Research Center at Edwards Air Force Base
4. Period of Performance:
90 days lead time after contract award.
File details come from the government source that posted it. Updated .