Mission System Design Engineer

Flight Control Systems Engineer

Embedded Software Engineer

Avionics Engineer

Responsibilities:&nbsp;<ul><li>Support all phases of development from initial proposal development through successful design, qualification, integration testing, flight test, and production.</li></ul> Specific experience with some or all of the following: <ul><li>Targeting, Weapons, EO/IR Sensors, Radars, HUD/HMD, Aircraft Survivability Equipment (ASE) and/or Autonomous Teaming</li><li>Communications Systems: VHF/UHF, SATCOM, TCDL, ICS</li><li>Navigation: EGI, GPS, IFF, ADS-B, TCAS, ILS, TACAN, Radar Altimeter, Air Data, TF/TA</li><li>Modular Open Systems Architectures, Model Based Systems Engineering, Open Standards (e.g. Future Avionics Capability Environment (FACE), Hardware Open Systems Technologies (HOST), Sensor Open System Architecture (SOSA))</li><li>Creation of system architecture and system schematics.</li><li>Creation of system performance specifications, interface control documents, and test plans/procedures.</li><li>Development of test requirements to drive systems integration lab and flight test aircraft instrumentation design</li><li>Perform hardware and software integration testing of multiple systems operating together in a systems integration lab&nbsp;&nbsp;</li></ul> Requirements:&nbsp;<ul><li>Bachelor's Degree in Electrical Engineering or Software Engineering preferred; Bachelor's degree in a Science, Technology, Engineering or Math (STEM) discipline required</li></ul> Position Requirements: <ul><li>Experience at all levels will be considered with a minimum of 8 years relevant experience; 10-14 years preferred.</li><li>Preferred experience in military platform avionics and mission system integration.</li><li>Experience with qualification to standards such as RTCA DO-160, MIL-STD-810, MIL-STD-883, MIL-STD-461, MIL-STD-464, RTCA DO-178, and RTCA DO-254,&nbsp;</li><li>Familiarity with System Safety Assessments and Failure Hazard Analysis</li></ul> Preferred skills: <ul><li>Demonstrated engineering intuition, critical thinking, comfort with ambiguity</li><li>Strong oral and written skills as this position involves working with a diverse team of experienced professionals; customers and suppliers</li><li>Coordinate between engineering teams, suppliers and customers.</li><li>Work collaboratively in multi-disciplinary teams to define cross-functional interfaces and conduct air vehicle level trade studies as designs move from concept to production</li><li>Collaborating with engineers from other disciplines to include electrical power, flight controls, propulsion, airframe structures, rotors, fuel, hydraulics and drive systems</li><li>Analyze and resolve hardware/software integration issues as they arise</li><li>Must be eligible for obtaining and maintaining a U.S. DoD Secret Clearance</li></ul>

Responsibilities: <ul><li>Understand and adhere to enterprise architecture principles and best practices</li><li>Developing web-based applications that interface with multiple SaaS components</li><li>Writing backend end business logic and integrating front end client UI with backend API’s</li><li>Understand overall infrastructure and success measures for designing and implementing architectures and solutions.</li></ul> Requirements: <ul><li>Bachelor of Science Degree is required</li><li>Major in Computer Engineering, Software Engineering, or Computer Science is preferred.</li><li>Bachelor’s Degree in Physics, Electrical, Aerospace, or Mechanical Engineering will be considered with sufficient software development experience.</li><li>Master’s Degree in the Engineering disciplines mentioned above is preferred.</li></ul> Position Requirements: <ul><li>Experience at all levels will be considered with a minimum of 2 years specific experience with flight controls, software, avionics, or electrical systems integration, development, and testing.</li><li>Familiarity with RTCA DO-160, MIL-STD-810, RTCA DO-178, RTCA DO-254, SAE ARP4754A, SAE ARP4761, 14 CFR Part 27 and Part 29 for commercial and military qualification and certification of aircraft systems.</li><li>Experience with Primary Development Environment:</li><li>MathWorks MATLAB / Simulink with Stateflow and Embedded Coder</li><li>C/C++ code</li><li>C# test scripts</li><li>IBM Rational DOORS</li><li>Serena Dimensions / PVCS</li><li>Git</li><li>Mentor Graphics Capital Harness System</li></ul>

Responsibilities: <ul><li>Duties include analyzing, designing, coding and code modification (typically in C/C++) of software designs of airborne embedded software implementations.</li><li>Participate in requirements management via DOORS, systems specifications, and interface management.&nbsp;&nbsp;</li><li>Manage software lifecycle data via DIMENSIONs configuration management tool.</li><li>Generate software requirements to integrate avionics sensors and equipment (i.e. engines, ARINC429, hydraulics, electrical systems, landing gear, RS-422, analog signals, discretes, CAN Bus, etc.)</li><li>Assist in the evaluation of software designs to identify design flaws.</li><li>Utilize a Windows and MOSA based software development environment.</li><li>Assist in the verification and validation testing of airborne embedded software using a desktop simulation environment, systems integration labs, surrogate platforms flight testing and aircraft flight testing.</li></ul> Requirements:&nbsp; <ul><li>Bachelor's Degree is required.</li><li>Major in in Computer Science, Electrical or Aerospace Engineering is preferred.&nbsp;</li><li>Applied Sciences (Physics) or Mechanical Engineering may be considered with applicable embedded software experience.</li></ul> Position Requirements:&nbsp; <ul><li>At least 5 years of relevant software experience, preferably in aerospace industry.</li><li>Ability to develop software in a RTOS environment.</li><li>Interest with ARINC653 software specification for space and time partitioning in safety-critical avionics real-time operating systems (RTOS)</li><li>Skilled in utilizing modern programming languages (e.g. C++, C#, Java, Python).</li><li>Skilled with embedded software development on Multicore processors.</li><li>Motivated person with strong problem-solving abilities, willingness to perform a wide variety of related tasks.</li><li>Effective communication skills (both verbal and written).</li><li>Interest in modern airborne sensors, avionics, mission systems, weapons systems, or electrical systems integration, development, and testing.</li><li>Familiarity with commercial certification and military qualification of aircraft systems is advantageous.</li><li>Experience with Eclipse based software is advantageous (most chip vendors and software vendors are moving to this IDE. TI-CodeComposer, NXP-CodeWarrior, DDC-I OpenArbor, etc.).</li><li>Linux/Unix experience (simple commands like ls (in windows dir), rm (del a file), md, cd, rd (make directory, change directory and remove directory) man – the builtin help documentation.</li><li>Software repositories – GiT , Tortoise GiT or some other tool that has been wrapped around GiT.</li><li>Experience with DO-178B/C software development lifecycle guidelines – Software Considerations in Airborne Systems and Equipment Certification (and the DO-178C supplements).</li><li>Interests with the integration of the Army’s Future Airborne Capability Environment (FACE) on vertical lift vehicles.</li></ul>

Responsibilities: <ul><li>Design and test of Avionics &amp; Electrical Systems with integration of complex software and hardware, including Electrical Power Generation and Distribution Systems, Integrated Avionics Systems and Displays, Communication and Navigation Systems, Mission Equipment Integration, Sensors and Vehicle Health Monitoring Systems.</li><li>System and software design, requirements management, systems specifications, interface management, system safety assessment, verification and validation testing in desktop simulation environment and systems integration labs, aircraft flight test, and aircraft/system qualification and certification.</li></ul> Requirements: <ul><li>Bachelor’s Degree is required; Major in Electrical Engineering, Computer Engineering, or Software Engineering is preferred and Bachelor’s Degree in Physics, Computer Science, Aerospace, or Mechanical Engineering will be considered.</li><li>Master’s Degree in the Engineering disciplines mentioned above is preferred.</li></ul> Position Requirements: <ul><li>At least 6 year’s experience directly related to the responsibilities of this position.</li><li>Experience with flight controls, software, avionics, or electrical systems integration, development, and testing.</li><li>Familiarity with RTCA DO-160, MIL-STD-810, RTCA DO-178, RTCA DO-254, SAE ARP4754A, SAE ARP4761, 14</li><li>CFR Part 27 and Part 29 for commercial and military qualification and certification of aircraft systems</li><li>Experience with Primary Development Environment is preferred</li><li>MathWorks MATLAB / Simulink with Stateflow and Embedded Coder is preferred</li><li>C/C++ code experience preferred</li><li>C# test scripts experience preferred</li><li>Git experience preferred</li></ul>

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4 wichita Jobs found

Mission System Design Engineer

Flight Control Systems Engineer

Embedded Software Engineer

Avionics Engineer

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4 wichita Jobs found

Mission System Design Engineer

Flight Control Systems Engineer

Embedded Software Engineer

Avionics Engineer

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