Avionics

Aircraft electrical systems distribute reliable AC and DC power to flight-critical and utility loads with redundancy.

Navigation systems combine ground aids, inertial sensing, and satellite positioning for continuous aircraft guidance.

Aircraft communication systems are designed through link-budget analysis of power, path loss, bandwidth, and modulation constraints.

Flight instruments convert pressure, inertial, and magnetic sensing into pilot-ready speed, altitude, attitude, and heading information.

Fly-by-wire systems replace mechanical linkages with electronically commanded, redundancy-protected closed-loop control laws.