Todd Krieger
 6356 W. Villa Rita Dr., Glendale, AZ 85308 (602) 738-1469

ENGINEER- Software Test, Software Development, System Test. DO-178B. Real-time
embedded. LDRA. VectorCAST. Aerospace.

TECHNICAL BACKGROUND:
 Software Development and Test: Programming Languages: C, C++, Ada.
 Software quality, architecture, and requirements. Verification and
 validation. Object-oriented design. Real-time Embedded using VxWorks.
 ATE, unit test, and integration. Digital Signal Processing. DO-178B
 and MIL-STD-498 standards. LDRA, VectorCAST, and McCabe structural
 coverage and analysis. Test scripts. Requirements traceability.
 Operating Systems: Windows NT/2000/ME/XP, DEC VAX VMS, and UNIX (Linux, AIX,
Solaris).

 Configuration Management: Rational ClearCase and ClearQuest, PCVS.

 Electronics Hardware: Peripheral electronics for microprocessor-based
 systems. TTL and CMOS circuitry. Printed Circuit Board design.
 Analog, digital, and integrated electronics. System controls,
 response, and feedback. MIL-specs and commercial hardware. ATE
 hardware/interface, UL/CSA specifications. Actuators and sensors.

 General: Hardware-software integration and test. Microsoft Office
 documentation.

JOB HIGHLIGHTS:
 Rogerson/Kratos, Pasadena, CA. Contract through Oxford Global Resources, March
2009 to June 2009.
 Testing and qualification for the Bell Helicopter 429 DU Navigational
 Displays. Verification and validation of requirements, failure  
 analysis, ARINC 429 protocols, McCabe coverage analysis, trace 
 coverage, coding standards (C/C++), and updating of test procedure  
 documentation.

 ENEA/TekSci, Tempe, AZ. Contract March 2005 to Jan 2009.
 Testing and structural coverage for the Boeing C-17 Core Integrated
 Processor (CIP) software. Testing utilized LDRA Testbed and TBrun for
 structural coverage verification (DO-178B Level B and Level C) for
 upgraded software. Testing involved Ada and C/C++ software on UNIX
 platform (Greenhills compiler), interfacing with LDRA on Windows XP
 platform. Integration Test and Documentation for new ARINC-429
 functionality.
 Testing and structural coverage for the Honeywell RDR-4000 Aircraft
 Weather Radar control electronics. DO-178B based testing of software
 running the I/O and signal processor units. Utilized VisionClick and
 LDRA platforms for software verification per requirements and
 complete coverage of the latest code release.

 Honeywell, Commercial Aircraft Systems, Glendale, AZ; Air Transport
 Systems, Phoenix, AZ.
 Contract September 2000 to February 2002; direct March 2002 to September 2003;
contract May 2004 to March 2005.
 Digital Radio Systems for commercial aircraft. Developed software and
 test methods for the voice and avionics data radios. DSP software for
 Digital Radios. Constructed databases (Microsoft Access) and test
 procedures to define radio functionality. Test scripts (C, MS
 Visual Basic) for the real-time embedded software. DO-178B Level A
 verification using VisionClick platform. Upgraded software for the
 Boeing 777 AIMS flight deck data communications.

 Manpower Technical, Tucson, AZ. Contract February 1999 to August 1999.
 Raytheon Standard Missile LEAP KW Test Station. Developed the
 exception handler (ANSI C/Windows NT) for the real-time embedded 
 flight software, to override the existing VxWorks exception  
 handler.  The replacement exception handler prevented automatic 
 reboot of the Motorola PowerPC processor during critical flight.

 Honeywell, Satellite Systems Operation, Glendale (Phoenix), AZ. Contract 1996
to July 1998.
 Multiplexer-Demultiplexer Applications Test Environment (MATE) data
 communications simulator for the International Space Station. System
 consists of a DEC VAX-based hardware controller, a Sun SPARCstation
 (UNIX) simulator-controller, a VME-based communication system, and 
 PC-based Utilities Platform. The VAX and Sun coordinate the system 
 data transfers to run simulations, communications, and data tests  
 via the VME interface. Software unit test- C, C++, and Ada on the 
 Solaris and AIX UNIX platforms.

 Rockwell, Collins Division, Cedar Rapids, IA. Contract June 1992 to
 September 1995.
 Manual and automated test equipment (ATE) for the Miniature Airborne
 GPS Receiver, the SDU 900 Series Voice/Data Satellite Communications
 Receiver, and the ARINC-429 Resource Module. Electronics control and
 interface circuitry, IEEE-488/GPIB control software, and direct I/O.
 Developed real-time embedded software (MetaWare C++) for the ARINC 
 429 Resource Module (VXI module with Intel 80486 processor) using the
 MicroTek Debugger and 486 In-Circuit Emulator.

 General Electric Company, Philadelphia, PA. Contract February 1991 to
 August 1991.
 Test Simulator Unit for the White Sands Satellite Ground Station.
 Developed electronics and software (Microsoft C); and tested proper
 function of the automated control module. Authored test 
 documentation. System also incorporated self-tests using IEEE-488 
 based PC-controlled ATE.

 Rockwell, North American Aircraft, Palmdale, CA. June 1985 to March
 1990.
 Testing, troubleshooting, modification, and repair of 
 line-replaceable units (LRUs) for the B-1B Bomber. LRUs included 
 electromechanical power-control assemblies (PCAs), signal-
 conditioning and multiplexing units, flight control units, serial-
 digital multiplex assemblies (SDMAs), and avionics. Manual and 
 automated test. Authored procedures for numerous
 tests for defect verification. Worked on software (PASCAL) for 
 multiplex unit ATE.

EDUCATION: Case Western Reserve Univ., Cleveland, OH. Bachelor of
 Science, Electrical Engineering. 1985.

References available upon request.