Bahri, S.Sasongko, R. A.2022-03-302022-03-3020181742-6588https://depositonce.tu-berlin.de/handle/11303/16607http://dx.doi.org/10.14279/depositonce-15384The implementation of Flight Control Law (FCL) for Aircraft Electronic Flight Control System (EFCS) aims to reduce pilot workload, while can also enhance the control performance during missions that require long endurance flight and high accuracy maneuver. In the development of FCL, a quantitative representation of the aircraft dynamics is needed for describing the aircraft dynamics characteristic and for becoming the basis of the FCL design. Hence, a 6 Degree of Freedom nonlinear model of a light utility aircraft dynamics, also called the nonlinear Flight Mechanical Model (FMM), is constructed. This paper shows the construction of FMM from mathematical formulation, the architecture design of FMM, the trimming process and simulations. The verification of FMM is done by analysis of aircraft behaviour in selected trimmed conditions.en530 Physiknonlinear flight mechanical modelhigh aspect ratio light utility aircraftFCLEFCSAircraft Electronic Flight Control SystemArticle2022-03-271742-6596