Module Code: MECH 5765M01 1. Analyse and formulate the requirements in the following questions. a. In the process of designing an aircraft stability control system, you are tasked with selecting the best IMU (Inertial Measurement Unit) that is suitable to satisfy the following requirements: "The aircraft shall be capable of measuring its roll and pitch with an accuracy of 0.01 and 95.4% confidence". Refer to the IMU options in table Q1.1 and explain your choice. [7 marks] Table Q 1.1: List of datasheet quoted accuracy for three Inertial Measurement Unit options. IMU IMU1 IMU2 IMU3 Accuracy 0.01 0.01 0.01 Quoted Accuracy type 1-Standard Deviation Root Mean Square 3-Standard Deviation