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True Anomaly

Builds spacecraft and software for space defense

GNC Engineer - Missile Defense

Flight Dynamics & GNCConfirmed live in the last 24 hours
Full-time

About the Job

Requirements

  • A bachelor's degree in aerospace engineering, mechanical engineering, electrical engineering, physics, or a related field is required.
  • At least 5 years of relevant GNC engineering experience in the aerospace and defense industry is required; experience with tactical missile systems, interceptors, or guided munitions is preferred.
  • Coursework or project experience in flight dynamics, aerodynamics, control systems, and state estimation is required.
  • A strong understanding of physics, rigid body dynamics, intercept geometry, proportional navigation, and real-time software development principles is required.
  • Experience with C++ and/or Python for algorithm development, numerical methods, real-time control, or simulation is required.
  • Familiarity with missile GNC concepts, including guidance laws, autopilot design, sensor fusion, inertial navigation, seeker operation, and aerodynamic or thrust vector control, is required.
  • Exposure to filtering and estimation methods, such as Kalman filters, complementary filters, and INS/GPS integration, through internships, coursework, or projects is required.
  • Ability to build, test, and debug flight software, real-time control systems, and simulation tools is required.
  • Strong analytical skills emphasizing dynamics, controls, and numerical methods are required.
  • Ability to work effectively in a fast-paced, multidisciplinary engineering environment is required.
  • Demonstrated ability to take ownership of complex technical problems and drive solutions from concept through flight test is required.
  • Ability to obtain and maintain a Top Secret/Sensitive Compartmented Information U.S. government security clearance is required.

Responsibilities

  • Own all aspects of Guidance, Navigation, and Control system development for missile systems, including architecture definition, algorithm design, verification, hardware integration, flight test support, and operational deployment.
  • Design, test, and validate GNC flight software and embedded algorithms for missiles operating across multiple flight regimes and environmental conditions.
  • Develop and maintain navigation and state estimation algorithms, including sensor fusion frameworks such as extended Kalman filters, unscented Kalman filters, and particle filters, integrating inertial measurement unit, GPS/INS, seeker data, and other sensor modalities to provide high-rate, high-accuracy state estimates throughout the engagement timeline.
  • Develop guidance laws, including proportional navigation, augmented proportional navigation, and optimal guidance, and autopilot designs; implement them in flight software; and verify performance and robustness through high-fidelity six-degree-of-freedom simulation, Monte Carlo analysis, hardware-in-the-loop testing, and flight test correlation.
  • Design, implement, and maintain high-fidelity simulation environments capturing aerodynamics, propulsion, atmospheric effects, target dynamics, sensor models, and actuator dynamics for software-in-the-loop, hardware-in-the-loop, and mission analysis across the full flight envelope.
  • Use frequency-domain and time-domain control analysis techniques to ensure stability margins.
  • Develop terminal guidance algorithms for intercepting maneuvering targets, including target tracking, aimpoint selection, miss distance prediction, time-to-go estimation, and endgame steering logic.

Desired Qualifications

  • A master's degree or PhD in aerospace engineering, control systems, or an equivalent discipline is preferred.
  • Experience with terminal guidance algorithms, proportional navigation variants, optimal guidance theory, or modern guidance techniques is preferred.
  • Experience developing autopilot designs for agile missiles, including gain scheduling, adaptive control, or nonlinear control methods, is preferred.
  • Experience with INS/GPS integration, sensor calibration, alignment algorithms, and error budget analysis is preferred.
  • Experience with aerodynamic modeling, computational fluid dynamics correlation to flight data, or aeroservoelastic analysis is preferred.
  • Experience developing and executing hardware-in-the-loop test campaigns with flight-representative GNC hardware is preferred.
  • Flight test experience, including test planning, instrumentation selection, telemetry analysis, and flight data reconstruction, is preferred.
  • Experience with intercept kinematics, target tracking, miss distance analysis, and covariance propagation is preferred.
  • Experience performing line-of-sight stability analysis, including jitter, noise rejection, and seeker tracking performance, is preferred.
  • Hands-on experience with GNC hardware integration, sensor characterization, and actuator calibration is preferred.
  • Familiarity with missile-specific tools and standards, including MISSILE DATCOM, MIL-STD-1553, and MIL-STD-1760, is preferred.
  • An active Top Secret/Sensitive Compartmented Information clearance with polygraph is preferred.

About the Company

True Anomaly

Builds spacecraft and software for space defense

True Anomaly builds spacecraft and mission software for US and allied defense organizations operating in space. Its Jackal autonomous orbital vehicle carries sensors that detect, track and image other spacecraft, then maneuvers to perform rendezvous and proximity operations. Operators use Mosaic to plan missions, simulate maneuvers, send commands and review data from satellites and ground systems while retaining control over autonomous actions. The company develops and manufactures its hardware in the United States and supplies spacecraft, payloads and software through defense programs and contracts. True Anomaly was founded in 2022 and is headquartered in Centennial, Colorado.

Company size
201-500
Company stage
Debt Financing
Total funding
$1B
Headquarters
Centennial, CO
Founded
2022

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