In this paper, we explore fuzzy logic based approach for lateral control of aircrafts. Here the effect of roll on yaw and that of yaw on roll is taken into account. So the system will have greater accuracy and efficiency than the application of two separate controllers. This design will significantly reduce instability and increases maneuverability, as compared to existing control systems.
|Number of pages||13|
|Specialist publication||Sensors and Transducers|
|Publication status||Published - 2012|
All Science Journal Classification (ASJC) codes
- Control and Systems Engineering
- Electrical and Electronic Engineering