Commander, Naval Air Warfare Center Weapons Division, Code 210000D, 1 Administration Circle, China Lake, CA 93555-6100

70 -- SOFTWARE DEBUGGER AND PERFORMANCE MEASURING SYSTEM (SDPM) SOL N68936-99-R-0147 POC Derrick Hu, Contract Specialist, (760) 939-9655 This is a combined synopsis/solicitation for commercial items prepared in accordance with the format in Subpart 12.6, as supplemented with additional information included in this notice. This announcement constitutes the only solicitation; proposals are being requested and a written solicitation will not be issued. N68936-99-R-0147 is issued as a request for proposal. The solicitation document and incorporated provisions and clauses are those in effect through Federal Acquisition Circular 97-11. The Naval Air Warfare Center Weapons Division, China Lake, CA intends to procure one (1) Software Debugger and Performance Measuring System (SDPM). The system shall provide real time software debugging and performance measuring capability for the F/A-18 Mission Computer (MC). The AN/AYK-14 mission computer was designed by Control Data Corporation and is used in the F/A-18 aircraft. The specific F/A-18 MC targeted for instrumentation with the Software Debugger and Performance Measuring (SDPM) system is known as the AN/AYK-14 (v), XN-8, VPM-25B. The XN-8 computer contains (2) two VHSIC Processor Module (VPM) CPUs and (6) six MIL-STD-1553 DSMs. The SDPM system must interface with (2) VPMs and (2) DSMs in the XN-8 configuration. The SDPM must provide an off-the-shelf capability to non-intrusively monitor the MC in real time and allow simultaneous bus monitoring of two buses. Non-intrusive is defined for the purpose of this specification as a device that provides the capability described above without the use of the target computers memory, registers, or CPU. The SDPM shall not inject wait states, cycle stealing, or affect software timing or sequencing during the monitoring function. The SDPM system must provide the capability to monitor (2) two MC configurations simultaneously. All channels being monitored will use a common time stamp to allow correlation of data collected from multiple channels and/or multiple bus channels. The SDPM system must include the all hardware, modules, and cables necessary to perform testingof the AN/AYK-14, XN-8, VPM-25B computer. Capabilities that must be provided are: symbolic debugging, automated symbol table translation, trace, performance profiling, selective data logging, and event detection. The device must also provide the capability to time tag events and provide statistics of back plane traffic usage. Test setup, control, and post-run analysis should be accomplished with a symbolic user interface to increase user productivity. Graphical analysis software should be provided to plot variable data and profile bus traffic quickly and easily. Detailed minimum requirements are: Modes of operation -- Real time display of specified variables; continuous recorded trace of user specified events; delayed triggering for pre, center, and post trigger events; ability to record and display which code and data locations were accessed during the testing. Real-time for the purpose of the specification is defined as testing that provides immediate response to events and display results to the testeras the events occur. The SDPM must be capable of a sustained recording rate of more than 40,000 events per second during the log mode. The unit must be capable of recording up to 250 unique addresses and provide the capability to trigger on the nth occurrence of an event, the difference count between two events, the delta time between two events or the elapsed time from one event. The device must have provisions to execute user specified actions upon the occurrence of the conditions described in the preceding sentence. The contractor shall provide a user's manual which gives adequate instructions for installation, operation and routine maintenance. The contractor shall provide all software necessary to enable the system to perform in accordance with the above specifications and requirements. The contractor shall provide any standard commercial warranty for the above described device. Interface specifications must comply with those described in MDC-A3818 F-18 Avionics Multiplex Design Specifications dated 15 March 1976, MDC-A5690 F-15 Avionics Specification Commensurate with MIL-STD-1553B dated 21 Sept. 1978. Delivery shall be made FOB Destination 60 days from date of award to the following address: COMMANDER, Code 457100D, Bldg. 20291, 1 Administration Circle, China Lake, CA 93555-6100. The provisions at 52.212-1 applies to this acquisition. Past performance information should be submitted with proposal and include recent and relevant contracts for the same or similar items and other references (including contract number, points of contact with telephone numbers and other relevant information). Offerors shall include a completed copy of the provisions at FAR 52.212-3 and DFARS 252.212-7000. FAR clause 52.212-2 applies to this acquisition. The evaluation factors included in 52.212-2(a) include Technical, Price, and Past Performance. FAR clause 52.212-4 and 52.212-5 (52.203-6, 52.219-8, 52.222-26, 52.222-35, 52.222-36, 52.222-37, 52.225-3, 52.225-18, 52.225-19, 52.225-21, 52.222-33, and 52.247-64), and DFARS 252.212-7001 (252.225-7001, 252.225-7012, 252.225-7014, 252.225-7015, 252.225-7036, 252.227-7015, 252.227-7037, 252.243-7002, and 252.225-7014), and 252.212-7004 apply to this acquisition. The closing date for this solicitation/synopsis is 30 days from the date the solicitation/synopsis appears in the CBD. If you need a copy of the specifications noted above, or have any questions regarding this solicitation, contact Derrick Hu, Contract Specialist at (760) 939-9655 or Diane Foucher, Contracting Officer at (760) 939-8160. Posted 07/08/99 (I-SN351786). (0189)

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