Abstract
Presently, controlling of an aircraft system is quite complex due to huge variations in the number of aircraft flying in the space, environment, etc. The control system and aircraft community jointly work together hardly to stabilize and control the aircraft system under the various operating conditions. Following the works of control system community, the current paper concentrates on designing hybrid control techniques such as (i) switched linear control system and (ii) coordinated and uncoordinated control inputs for the aircraft Yaw and roll control system. The modelling begins with a derivation of suitable mathematical model to describe the lateral dynamic motion of the aircraft. Later, the proposed control techniques are validated by simulating under various conditions in MATLAB/SIMULINK platform, and the results are compared and tabulated with each other.
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Pavithra, A.C., Archana, N.V. (2022). Hybrid Control Design Techniques for Aircraft Yaw and Roll Control System. In: Raj, J.S., Shi, Y., Pelusi, D., Balas, V.E. (eds) Intelligent Sustainable Systems. Lecture Notes in Networks and Systems, vol 458. Springer, Singapore. https://doi.org/10.1007/978-981-19-2894-9_34
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DOI: https://doi.org/10.1007/978-981-19-2894-9_34
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