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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Support development of mathematical models to simulate flight of Aeroelastic aircraft.
- Develop & Evaluate guidance laws for flight path optimization and energy management.
- Support control law development for aeroelastic aircraft.
- Execute SIL, PIL and HIL simulations.
- Develop estimators/Filters.
- Support control surface sizing and evaluation of control surface effectiveness across the flight envelope.
- Perform ground testing to evaluate performance of FCS elements.
- Support flight testing and post flight analysis of FCS for aeroelastic aircraft.
- Documentation of work to build the knowledge base of the company.
- Execute tasks independently and be responsible for deliverables.
- Support team members to meet project requirements & deadlines.
Must have skills:
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2+ years of experience in flight dynamics modeling, flight simulation development and/or control law design.
- Strong foundation in flight mechanics, mathematical modeling, and fundamentals of guidance, navigation and control.
- Solid foundation in Control law design (or) estimator filter design, (or) development of guidance algorithms.
- Familiarity with aeroelasticity and implications on flight control systems is preferred.
- Flight test experience for FCS evaluation is preferred.
- Control system design using MATLAB, Simulink and other tools.
- Strong interpersonal and communication skills.
- Creative problem solving and analytical skills.