Benjamin Bowman

System Engineer at FTS International, LLC
  • Claim this Profile
Contact Information
us****@****om
(386) 825-5501
Location
Washington DC-Baltimore Area Contact Info

Topline Score

Topline score feature will be out soon.

Bio

Generated by
Topline AI

You need to have a working account to view this content.
You need to have a working account to view this content.

Experience

    • United States
    • Defense and Space Manufacturing
    • 1 - 100 Employee
    • System Engineer
      • Feb 2021 - Present

    • United States
    • Defense and Space Manufacturing
    • 100 - 200 Employee
    • System Engineer
      • Sep 2016 - Sep 2020

      Technical lead for high fidelity SIGINT system simulator

    • Defense & Space
    • 100 - 200 Employee
    • Systems Engineer
      • May 2014 - Sep 2016

      Chantilly, VA Authored matlab code for phased array and interferometer modeling

    • United States
    • Higher Education
    • 700 & Above Employee
    • Eric A. Walker Graduate Research Assistant
      • May 2012 - May 2014

      Masters Paper: An In-Flight Attitude Alignment Correction Method for Undersea Vehicles. Abstract - A method and criteria for correction of navigation roll and pitch angle error sustained during launch initiation and accumulated from drift due to intrinsic IMU rate gyro bias is presented for small, compact, high performance forward flight Undersea Vehicles (UVs). Normal periodic steady level flight (SLF) legs executed during mission transit to a target are advantageously used for correction… Show more Masters Paper: An In-Flight Attitude Alignment Correction Method for Undersea Vehicles. Abstract - A method and criteria for correction of navigation roll and pitch angle error sustained during launch initiation and accumulated from drift due to intrinsic IMU rate gyro bias is presented for small, compact, high performance forward flight Undersea Vehicles (UVs). Normal periodic steady level flight (SLF) legs executed during mission transit to a target are advantageously used for correction estimation. The correction is executed through the updating of the vehicle control Strapdown Inertial Navigation System (SINS) process in a single autopilot processor cycle step. NI LabVIEW programming for multiple single axis test evaluations of Inertial Measurement Units for use in underwater vehicles

    • Undergraduate Student
      • May 2009 - May 2012

      NI LabVIEW programming for development and improvement of Highly Accelerated Life Test (HALT) programs for acceptance testing

    • United States
    • Defense and Space Manufacturing
    • 300 - 400 Employee
    • Systems Engineer
      • 2014 - 2014

Education

  • Penn State University
    Master's Degree, Electrical Engineering
    2012 - 2014
  • Penn State University
    Bachelor of Science (B.S.), Electrical and Electronics Engineering
    2008 - 2012

Community

You need to have a working account to view this content. Click here to join now