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Cyient

Engineering -Flight Control Laws Design

Montreal, QC, Canada

Full-time

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Job details

Job type: Full-time
Apply by: Dec 4, 2026
Experience: You must have a minimum of 10 years of pertinent experience in the development of Flight Control Laws for FBW (Fly‑By‑Wire) aircraft
Posting language: English
Posted: Nov 4, 2026

Original job description

What are your contributions to the team?

Develop and improve both new and existing CLaws design as well the corresponding assessment tools using Matlab and C++ programming
Support CLaws, autopilot, and navigation design development for R&D projects
Develop CLaws and systems requirements
Perform CLaws requirements validation and verification (V&V) for any Claws updates and/or new Claws designs
Verify and deliver the CLaws in accordance with the DO‑178B standard and SAE ARP 4754
Design and develop pilot in the loop CLaws based on handling quality requirements, flight and structural envelope protection requirements, performance requirements, test pilot assessments and aircraft level requirements
Evaluate CLaws and FBW system failures, system stability and performance with analytical methods, desktop simulations, pilot in the loop simulator tests and flight test data
Support integration of CLAWS into various test rigs and supplier hardware (i.e. integrate into PFCC for Collins, Thales, NRC, CMC, etc)

How to thrive in this role?

You hold a bachelor’s or master’s degree in Aerospace Engineering, PhD degree is preferred in Aerospace Engineering
You must have a minimum of 10 years of pertinent experience in the development of Flight Control Laws for FBW (Fly‑By‑Wire) aircraft
You must be versed in aircraft flight dynamics with an in depth understanding of aerodynamics
You must be versed in "classical" and “modern” control systems design techniques for SISO and MIMO systems and be familiar with advanced control laws techniques and methods
You must have good understanding of control law evaluation techniques, linear and non‑linear and testing procedures
You must have a good understanding of aircraft stability, handling qualities, and control with a pilot‑in‑the‑loop
You should have a good understanding of DO‑178B standards, system requirements verification and validation methods and certification of complex software
You must be proficient in using Matlab and Simulink as a simulation, aircraft/system modeling and control law development tool
You should possess a good understanding of state estimation or Kalman filtering
You should be proficient in programming Matlab scripts and C++ programming
You must be fluent in written and spoken French and English
You must be a team player with an innovative spirit, motivated and be able to work independently

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More about this job

Responsibilities

Develop and improve flight control laws, autopilot and navigation designs, assessment tools, and system requirements for research and development projects. Validate and verify designs, assess aircraft and fly-by-wire system performance and failures, deliver compliant control laws, and support integration with test rigs and supplier hardware.

Requirements

Requires a bachelor's or master's degree in aerospace engineering and at least 10 years of experience developing flight control laws for fly-by-wire aircraft; a PhD is preferred. Candidates should have expertise in flight dynamics, aerodynamics, control systems, MATLAB/Simulink, C++, requirements verification and validation, and DO-178B, and be fluent in written and spoken French and English.

Skills

Flight Control Laws Design
Fly-By-Wire Aircraft
Aircraft Flight Dynamics
Aerodynamics
Control Systems Design
SISO and MIMO Systems
MATLAB
Simulink
C++ Programming
Requirements Development
Verification and Validation
DO-178B
SAE ARP 4754
Aircraft Stability and Handling Qualities
Kalman Filtering
Pilot-in-the-Loop Simulation

Visa sponsorship

Not detected in the job text

Keywords

Flight Control Laws
Fly-By-Wire
Autopilot
Navigation Systems
MATLAB
Simulink
C++
Aircraft Flight Dynamics
Aerodynamics
Classical Control Systems
Modern Control Systems
SISO
MIMO
Handling Qualities
Flight Envelope Protection
Structural Envelope Protection
Requirements Development
Requirements Verification and Validation
DO-178B
SAE ARP 4754
Aircraft Stability
Kalman Filtering
Pilot-in-the-Loop Simulation
Flight Testing
System Integration
Research and Development

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