Who we are:
We are a start-up based out of Bengaluru & Delhi NCR. We are engaged in development of next generation missions and technologies (NGM&T) towards future warfare needs of the Indian defence forces. It is undertaking research towards enhancing persistence and autonomy for unmanned vehicles and robotic swarms. NRT’s product development portfolio includes a solar power stratospheric high altitude pseudo satellite (HAPS) unmanned platform and an air/ground launched stand-off autonomous system.
Roles and Responsibilities:
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Establish processes for the development of the flight control system.
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Plan and execute test procedures for verification and validation of the flight control system.
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Develop mathematical models for simulating motion of flexible aircraft.
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Establish Flight control system architecture for aeroelastic aircraft.
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Control surface sizing and evaluating control surface effectiveness for aeroelastic aircraft.
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Control law development for aeroelastic modes and path stabilization.
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Develop advanced guidance algorithms for flight path optimization, jetstream crossing, thermal soaring and energy management.
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Develop estimators/ Kalman filters for estimating structural dynamic states.
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Create MATLAB code/ Simulink models to evaluate guidance, flight control and estimation algorithms
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Establish test setup for SIL, PIL and HIL simulations. Evaluate limitations and calibrate for errors.
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Post flight analysis and evaluation of Flight Control System.
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Prepare work breakdown plan for given problem statement.
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Coordinate with flight controls team and stakeholders to meet project requirements and deadlines
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Consistently and proactively work with team members to solve complex design problems.
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Guide team members for execution of project specific tasks.
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Good understaing of ROS/ROS2 and PX4 and avionics systems
Must have skills:
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5+ years of experience in flight dynamics modeling, flight simulation development, control law design, guidance law design (or) state estimator design.
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Knowledge of fundamental concepts of state estimation, guidance and flight control.
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Strong foundation in flight mechanics, mathematical modeling, and flight control design (or) state estimator design.
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Proven experience in developing flight control and guidance (or) state estimators/ kalman filters from concept to flight testing.
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Control system design using MATLAB, Simulink and other tools.
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Strong interpersonal and communication skills.
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Creative problem solving and analytical skills.
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C/C++/python
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Good Understanding of RPI / NVIDIA Jetson
Good to have skills:
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A sound understanding of aeroelastic flight dynamic modeling and control law development.
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Exposure to certification of flight control laws.
Basic Requirement (education & relevant experience):
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Bachelors or Masters in Aerospace/Aeronautical/Controls engineering with at least 1 degree in Aerospace/Aeronautical Engineering and minimum 5 years of experience