P Hušek, K Narenathreyas - Applied Soft Computing, 2016 - Elsevier
Fuzzy logic control of longitudinal motion of an aircraft based on Takagi–Sugeno modelling approach is presented in this paper. Takagi–Sugeno model of the motion along the desired …
U Ansari, AH Bajodah - Aircraft Engineering and Aerospace …, 2017 - emerald.com
Purpose To design a robust attitude control system for the ascent flight phase of satellite launch vehicles (SLVs). Design/methodology/approach The autopilot is based on …
JO Pedro, A Panday, L Dala - International Journal of Applied …, 2013 - sciendo.com
The paper presents the development of modelling and control strategies for a six-degree-of- freedom, unmanned combat aerial vehicle with the inclusion of the centre of gravity position …
U Ansari, AH Bajodah - … , Part M: Journal of Engineering for …, 2018 - journals.sagepub.com
A novel two-loop structured robust generalized dynamic inversion–based control system is proposed for autonomous underwater vehicles. The outer (position) loop of the generalized …
This paper presents the two-loops Robust Generalized Dynamic Inversion (RGDI) Quadrotor control system design. The outer loop of the system provides pitch and roll attitude …
The development of a two-loops Quadrotor's robust generalized dynamic inversion (RGDI)- based control system is presented. The outer (position) loop utilizes PD position control of …
Nonlinear Control of Robots and Unmanned Aerial Vehicles: An Integrated Approach presents control and regulation methods that rely upon feedback linearization techniques …
The nonlinear control problem of aircraft trajectory tracking is tackled in the framework of multiple linear time-varying constrained control using the newly developed paradigm of …
Abstract The Robust Generalized Dynamic Inversion (RGDI) homing guidance (HG) and control design methodology is proposed for intercepting highly maneuvering targets. The …