Iman Sadeghzadeh

发表

Fault-Tolerant Control of Quadrotor Helicopter Using Gain-Scheduled PID and Model Reference Adaptive Control

Youmin Zhang, Iman Sadeghzadeh, Ankit Mehta, 2016 .

Actuator fault-tolerant control based on Gain-Scheduled PID with application to fixed-wing Unmanned Aerial Vehicle

Iman Sadeghzadeh, Youmin Zhang, 2013, 2013 Conference on Control and Fault-Tolerant Systems (SysTol).

Control Allocation for a Modified Quadrotor Helicopter Based on Reliability Analysis

Youmin Zhang, Didier Theilliol, Iman Sadeghzadeh, 2012, Infotech@Aerospace.

Fault Tolerant Control of a Quadrotor Helicopter Using Model Reference Adaptive Control

Youmin Zhang, Iman Sadeghzadeh, Ankit Mehta, 2011 .

Payload Drop Application of Unmanned Quadrotor Helicopter Using Gain-Scheduled PID and Model Predictive Control Techniques

Youmin Zhang, Iman Sadeghzadeh, Mahyar Abdolhosseini, 2012, ICIRA.

Payload Drop Application Using an Unmanned Quadrotor Helicopter Based on Gain-Scheduled PID and Model Predictive Control

Youmin Zhang, Iman Sadeghzadeh, Mahyar Abdolhosseini, 2014 .

Fault Tolerant Flight Control of Unmanned AerialVehicles

Iman Sadeghzadeh, 2015 .

Control Allocation and Re-allocation for a Modified Quadrotor Helicopter against Actuator Faults

Youmin Zhang, Didier Theilliol, Iman Sadeghzadeh, 2012 .

Fault/Damage Tolerant Control of a Quadrotor Helicopter UAV using Model Reference Adaptive Control and Gain- Scheduled PID

Youmin Zhang, Iman Sadeghzadeh, Ankit Mehta, 2011 .

A Review on Fault-Tolerant Control for Unmanned Aerial Vehicles (UAVs)

Youmin Zhang, Iman Sadeghzadeh, Youmin Zhang, 2011 .

Active Fault Tolerant Control of a quadrotor UAV based on gainscheduled PID control

Youmin Zhang, Iman Sadeghzadeh, Ankit Mehta, 2012, 2012 25th IEEE Canadian Conference on Electrical and Computer Engineering (CCECE).

Linear Parameter Varying control synthesis: State feedback versus H∞ technique with application to quadrotor UA V

Didier Theilliol, Iman Sadeghzadeh, Abbas Chamseddine, 2014, 2014 International Conference on Unmanned Aircraft Systems (ICUAS).

Optimal reliability design for over-actuated systems based on the MIT rule: Application to an octocopter helicopter testbed

Youmin Zhang, Philippe Weber, Didier Theilliol, 2014, Reliab. Eng. Syst. Saf..