mapping the thrust and torques applied to the quadcopter to the PWM commands (PX4_Autopilot)
Hello,I’m trying to implement a simple Hardware-in-the-Loop (HITL) simulation using PX4 and the UAV Toolbox Support Package for PX4 Autopilots (using PX4 Host Target). Specifically, I’ve customized a different controller for the quadcopter. However, I’m having trouble understanding how to use the actuator_write block. I’ve read the documentation, which states that the input should be between -1 and +1. How can we map the thrust and torques applied to the quadcopter to the commands u? Thanks.Hello,I’m trying to implement a simple Hardware-in-the-Loop (HITL) simulation using PX4 and the UAV Toolbox Support Package for PX4 Autopilots (using PX4 Host Target). Specifically, I’ve customized a different controller for the quadcopter. However, I’m having trouble understanding how to use the actuator_write block. I’ve read the documentation, which states that the input should be between -1 and +1. How can we map the thrust and torques applied to the quadcopter to the commands u? Thanks. Hello,I’m trying to implement a simple Hardware-in-the-Loop (HITL) simulation using PX4 and the UAV Toolbox Support Package for PX4 Autopilots (using PX4 Host Target). Specifically, I’ve customized a different controller for the quadcopter. However, I’m having trouble understanding how to use the actuator_write block. I’ve read the documentation, which states that the input should be between -1 and +1. How can we map the thrust and torques applied to the quadcopter to the commands u? Thanks. px4, uav control MATLAB Answers — New Questions