Ali Zunair

Passionate aerospace engineer with a strong interest in flight dynamics and controls. Skilled in-Flight Dynamics, Flight Controls System, and System Identification. Seeking to apply my knowledge and experience to a challenging role in the field of flight dynamics and controls.

Design and Development of Machine Learning Neural Network based Algorithm for prediction of Attitude Hold Autopilot

• Generating an Algorithm which solves geometry of an aircraft and provide stability derivatives.
• Controller Design for a number of aircraft which will serve as a dataset.
• Training and Testing.
• Artificial Neural Network Design.
• Hyper Parameter Tunning of neural network for maximum possible accuracy.
  

Design And Implementation of Flight Control System in a MALE UCAV

• Flight Dynamics Modelling Using Analytical Method.
• Stability Augmentation System Design to improve Handling Qualities,
• Actuator Selection using Hinge Moments.
• Verification of UCAV design Using Xplane Flight Simulator.
• Autopilots Design Classical Feedback Method on Linear Model.
• Testing these autopilots on nonlinear model involving Software in the loop Simulation
  

System Identification Analysis to calculate Stability Derivatives from Flight Data

• Developed Equation of Motion Derivation
• Calculation of Forces and Moments
• Applied Least Squares Method (LSM) to find stability derivatives
• Stability Derivatives Analysis
• Data Comparison
• Aerodynamic Insights
• Validation and Accuracy Assessment
• Impact on Flight Dynamics
  

Design, Modelling and Simulation of a Quad Copter

• 6 DOF Nonlinear Simulation in Simulink.
• Mechanical Integration of Quadcopter using DJI F450 Frame
• Putting together the electronic parts and components required for the quadcopter to function.
• Flight Controller connection and Gain Tuning
• Stability Analysis using Mission Planner

Aero Vehicle Design of a Business jet aircraft 

• First iteration of conceptual design of a business jet aircraft is achieved using Raymer Statistical
• Weight Sizing
• Design Parameters Calculation (W/S, T/W, CL, CD)
• Wing Design
• Engine Sizzing
• Landing Gears Design
• Stability Analysis
• Aerodynamics
• Structural Analysis
  

Aircraft Performance Analysis of AN 140

• Cruise Speed and Range Analysis
• Takeoff and Landing Distances
• Climb Rate and Ceiling
• Fuel Efficiency
• Stall Speed Analysis
• Maneuverability and Handling
• Endurance and Mission Profiles
• Aerodynamic Characteristics
• Safety Margins