Asks for

The ad says“Ability to obtain and maintain TS/SCI US government security clearance”
The ad says“Develop guidance laws (proportional navigation, augmented PN, optimal guidance) and autopilot designs; implement them in flight software; verify performance and robustness through high-fidelity 6-DOF simulation, Monte Carlo analysis, hardware-in-the-loop testing, and flight test correlation.”
The ad says“Own all aspects of Guidance, Navigation, and Control (GNC) system development for missile systems, including architecture definition, algorithm design, verification, hardware integration, flight test support, and operational deployment.”
The ad says“Experience with C++ and/or Python for algorithm development, numerical methods, real-time control, or simulation”
The ad says“Develop and maintain navigation and state estimation algorithms, including sensor fusion frameworks (e.g., EKF, UKF, particle filters) integrating IMU, GPS/INS, seeker data, and other sensor modalities to provide high-rate, high-accuracy state estimates throughout the engagement timeline.”
The ad says“Own all aspects of Guidance, Navigation, and Control (GNC) system development for missile systems, including architecture definition, algorithm design, verification, hardware integration, flight test support, and operational deployment.”
The ad says“Utilize frequency-domain and time-domain control analysis techniques to ensure stability margins.”
The ad says“Own all aspects of Guidance, Navigation, and Control (GNC) system development for missile systems, including architecture definition, algorithm design, verification, hardware integration, flight test support, and operational deployment.”
The ad says“Own all aspects of Guidance, Navigation, and Control (GNC) system development for missile systems, including architecture definition, algorithm design, verification, hardware integration, flight test support, and operational deployment.”
The ad says“Develop guidance laws (proportional navigation, augmented PN, optimal guidance) and autopilot designs; implement them in flight software; verify performance and robustness through high-fidelity 6-DOF simulation, Monte Carlo analysis, hardware-in-the-loop testing, and flight test correlation.”
The ad says“Strong understanding of physics, rigid body dynamics, intercept geometry, proportional navigation, and real-time software development principles”
The ad says“Develop guidance laws (proportional navigation, augmented PN, optimal guidance) and autopilot designs; implement them in flight software; verify performance and robustness through high-fidelity 6-DOF simulation, Monte Carlo analysis, hardware-in-the-loop testing, and flight test correlation.”
The ad says“Own all aspects of Guidance, Navigation, and Control (GNC) system development for missile systems, including architecture definition, algorithm design, verification, hardware integration, flight test support, and operational deployment.”
The ad says“Develop and maintain navigation and state estimation algorithms, including sensor fusion frameworks (e.g., EKF, UKF, particle filters) integrating IMU, GPS/INS, seeker data, and other sensor modalities to provide high-rate, high-accuracy state estimates throughout the engagement timeline.”
The ad says“Strong understanding of physics, rigid body dynamics, intercept geometry, proportional navigation, and real-time software development principles”
The ad says“Develop guidance laws (proportional navigation, augmented PN, optimal guidance) and autopilot designs; implement them in flight software; verify performance and robustness through high-fidelity 6-DOF simulation, Monte Carlo analysis, hardware-in-the-loop testing, and flight test correlation.”
The ad says“Experience with C++ and/or Python for algorithm development, numerical methods, real-time control, or simulation”
The ad says“Strong understanding of physics, rigid body dynamics, intercept geometry, proportional navigation, and real-time software development principles”
The ad says“Strong understanding of physics, rigid body dynamics, intercept geometry, proportional navigation, and real-time software development principles”
The ad says“Develop and maintain navigation and state estimation algorithms, including sensor fusion frameworks (e.g., EKF, UKF, particle filters) integrating IMU, GPS/INS, seeker data, and other sensor modalities to provide high-rate, high-accuracy state estimates throughout the engagement timeline.”
The ad says“Utilize frequency-domain and time-domain control analysis techniques to ensure stability margins.”
The ad says“Develop and maintain navigation and state estimation algorithms, including sensor fusion frameworks (e.g., EKF, UKF, particle filters) integrating IMU, GPS/INS, seeker data, and other sensor modalities to provide high-rate, high-accuracy state estimates throughout the engagement timeline.”
The ad says“Own all aspects of Guidance, Navigation, and Control (GNC) system development for missile systems, including architecture definition, algorithm design, verification, hardware integration, flight test support, and operational deployment.”

Space is a warfighting domain. True Anomaly seeks those with the talent and ambition to build the technology that secures it.

OUR MISSION

True Anomaly delivers decisive capabilities for space superiority. We build autonomous spacecraft, advanced payloads, mission software, and space-based interceptors — enabling the U.S. and its Allies to secure the space environment and counter threats from the ultimate high ground.

OUR VALUES

Be the offset. We create asymmetric advantages with creativity and ingenuity.
What would it take? We challenge assumptions to deliver ambitious results.
It’s the people. Our team is our competitive advantage and we are better together.

BENEFITS & PERKS*

Best-in-class healthcare: 100% company-paid medical, dental, and vision coverage for you and your dependents, with HSA/HRA options
Generous time off: Flexible Time Off (FTO) for exempt employees, accrued PTO of up to 25 days for non-exempt employees, plus 12 paid holidays; Parental Leave; Sick Leave
Fuel for your day: Daily catered lunch and unlimited snacks for in-office employees
And more: 401(k) retirement plan, fitness reimbursement, and Dog Fridays
Equity participation: Equity is included as part of our total compensation package, giving you an opportunity to share in the company’s success.

*Do not apply to fixed term and temporary roles

RESPONSIBILITIES

Own all aspects of Guidance, Navigation, and Control (GNC) 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 (e.g., EKF, UKF, particle filters) integrating IMU, GPS/INS, seeker data, and other sensor modalities to provide high-rate, high-accuracy state estimates throughout the engagement timeline.
Develop guidance laws (proportional navigation, augmented PN, optimal guidance) and autopilot designs; implement them in flight software; verify performance and robustness through high-fidelity 6-DOF 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 SIL, HIL, and mission analysis across the full flight envelope.
Utilize frequency-domain and time-domain control analysis techniques to ensure stability margins.
Develop terminal guidance algorithms for intercept of maneuvering targets, including target tracking, aimpoint selection, miss distance prediction, time-to-go estimation, and endgame steering logic.

QUALIFICATIONS

Bachelor's degree in aerospace engineering, mechanical engineering, electrical engineering, physics, or related field
5+ years of relevant GNC engineering experience in the aerospace and defense industry, preferably with tactical missile systems, interceptors, or guided munitions
Coursework or project experience in flight dynamics, aerodynamics, control systems, and state estimation
Strong understanding of physics, rigid body dynamics, intercept geometry, proportional navigation, and real-time software development principles
Experience with C++ and/or Python for algorithm development, numerical methods, real-time control, or simulation
Familiarity with missile GNC concepts including guidance laws, autopilot design, sensor fusion, inertial navigation, seeker operation, and aerodynamic/thrust vector control
Exposure to filtering and estimation methods (e.g., Kalman filters, complementary filters, INS/GPS integration) through internships, coursework, or projects
Ability to build, test, and debug flight software, real-time control systems, and simulation tools
Strong analytical skills with emphasis on dynamics, controls, and numerical methods; ability to work effectively in a fast-paced, multidisciplinary engineering environment
Demonstrated ability to take ownership of complex technical problems and drive solutions from concept through flight test
Ability to obtain and maintain TS/SCI US government security clearance

PREFERRED SKILLS AND EXPERIENCE

Master's degree or PhD in aerospace engineering, control systems, or equivalent discipline
Experience with terminal guidance algorithms, proportional navigation variants, optimal guidance theory, or modern guidance techniques
Experience developing autopilot designs for agile missiles including gain scheduling, adaptive control, or nonlinear control methods
Experience with INS/GPS integration, sensor calibration, alignment algorithms, and error budget analysis
Experience with aerodynamic modeling, CFD correlation to flight data, or aeroservoelastic analysis
Experience developing and executing hardware-in-the-loop test campaigns with flight representative GNC hardware
Flight test experience including test planning, instrumentation selection, telemetry analysis, and flight data reconstruction
Experience with intercept kinematics, target tracking, miss distance analysis, and covariance propagation
Experience performing line-of-sight stability analysis including jitter, noise rejection, and seeker tracking performance
Hands-on experience with GNC hardware integration, sensor characterization, and actuator calibration
Familiarity with missile-specific tools and standards (e.g., MISSILE DATCOM, MIL-STD-1553, MIL-STD-1760)
Active TS/SCI clearance with Polygraph

COMPENSATION

Base Salary: $115,000 - $300,000
Equity + Benefits including Health, Dental, Vision, HRA/HSA options, PTO and paid holidays, 401K, Parental Leave

Your actual level and base salary will be determined on a case-by-case basis and may vary based on the following considerations: job-related knowledge and skills, education, location, and experience.

ADDITIONAL REQUIREMENTS

Work Location—This is an onsite position, Successful candidates will be located near Denver, CO or Long Beach, CA
Work environment—the work environment; temperature, noise level, inside or outside, or other factors that will affect the person's working conditions while performing the job.
Physical demands—the physical demands of the job, including bending, sitting, lifting and driving.

This position will be open until it is successfully filled. To submit your application, please follow the directions below.

#LI-Onsite

To conform to U.S. Government space technology export regulations, including the International Traffic in Arms Regulations (ITAR) you must be a U.S. citizen, lawful permanent resident of the U.S., protected individual as defined by 8 U.S.C. 1324b(a)(3), or eligible to obtain the required authorizations from the U.S. Department of State.

True Anomaly is committed to equal employment opportunity on any basis protected by applicable state and federal laws. If you have a disability or additional need that requires accommodation, please do not hesitate to let us know.

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