View Video Presentation: https://doi. org/10.2514/6.2023-3798. vid This paper presents a
technique for designing an adaptive nonlinear controller for the pitch rate of the Cessna …

This paper presents a new control law based on type-2 fuzzy logic system (T2FLS) for the
Cessna Citation X aircraft during cruise. This methodology combines three control systems …

Abstract An accurate Unmanned Aerial System (UAS) Flight Dynamics Model (FDM) allows
us to design its efficient controller in early development phases and to increase safety while …

This paper presents a technique for designing a robust pitch controller using a C* control
architecture, and implementing adaptive methods for the longitudinal control of the Cessna …

Aerial Traffic Management (ATM) and Aerial Collision Avoidance (ACA) are the most
important issues in aviation transportation. Accurate Aircraft Trajectory Prediction (ATP) …

This paper proposes an adaptive boundary sine cosine optimizer with population reduction.
It is designed specifically to calculate an upper bound on the worst-case gain of a known …

This work outlines a method for designing an adaptive nonlinear controller for the lateral
control of the Cessna Citation X business aircraft. The objective of the proposed controller is …

This research presents a technique for designing an adaptive nonlinear controller for the
pitch rate of the Cessna Citation X business jet aircraft. The proposed control algorithm …

In recent years significant effort was put into developing analytical worst-case analysis tools
to supplement the Verification & Validation (V&V) process of complex industrial applications …

Simulating an aircraft model using of high fidelity models of subsystems for its primary and
secondary flight control actuators requires measuring or estimating aero-load data acting on …