Vetted SpecialistsExample profileAnjali S.Launch Vehicle GNC EngineerOwned the ascent attitude controller and TVC allocation for a small-lift launch vehicle across three flights; gain schedule and bending-mode filters held margins above 6 dB and 30 degrees through max-Q on every flightBuilt and maintained the 6-DOF dispersed Monte Carlo (5,000-case runs across mass properties, winds, engine performance and IMU error) that fed the flight-safety data package for range approvalReduced first-stage insertion error by 40% by redesigning the closed-loop guidance update and validating it against post-flight telemetryAscent control6-DOF Monte CarloTVC allocation
Vetted SpecialistsExample profileNathan R.Spacecraft GNC and Attitude Determination EngineerDesigned the attitude determination and control system for a 12-satellite LEO constellation: EKF fusing star tracker, IMU, magnetometer and sun sensors, reaction wheel control and magnetorquer momentum managementDelivered pointing knowledge of 15 arcseconds against a 30-arcsecond requirement, verified on orbit across the first six vehiclesWrote the orbit maintenance and collision-avoidance maneuver planning tool now used by the operations team, cutting maneuver planning from two days to four hoursADCSKalman filteringOrbit design
Vetted SpecialistsExample profileCamila A.Autonomous Aircraft GNC EngineerGNC lead for a Group 3 UAS: inner-loop attitude control, L1 path following, wind estimation and an EKF-based navigation filter that held position within 30 meters over 20 minutes of GNSS-denied flightStood up the hardware-in-the-loop bench (flight computer, sensor emulation, actuator loads) and ran 400+ HIL cases per software release before flight testSupported 60+ flight-test sorties with real-time telemetry review, post-flight system identification and model updates that closed the sim-to-flight gapGNSS-denied navHILFlight test