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Conceptual design procedure of Unmanned Aerial Vehicle (UAV) flight control system is discussed in this paper. Detailed discussion of important aspects of UAV relating to its role, mission, capabilities and their implications on the flight control system are discussed. This leads to the basic requirements for the flight control and then translates to the type of controller to be used on board the...
An improved core algorithm is proposed for ldquoTotal Energy Control Systemrdquo(TECS), which diminishes the response oscillations caused by the cooperation error between aircraft total energy and its distribution. The construction of a feedback loop based on energy cooperation error to enhance decoupling performance for airspeed and flight path angle is the key step in the proposed approach. Based...
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