This paper proposes a Lyapunov based model reference adaptive PD/PID controller for
Satellite Launch Vehicle (SLV) systems. SLV is an open loop unstable plant with time …

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 …

In this paper, the attitude tracking and load relief control problems against wind disturbances
and uncertain aerodynamics as well as the engine thrust of launch vehicles are studied …

This paper presents a generalized dynamic inversion attitude control design for satellite
launch vehicle. Dynamic constraints that encapsulate the attitude tracking objectives are …

This paper presents the robustified form of generalized dynamic inversion control and its
application to attitude control for satellite launch vehicle. In proposed control law, dynamic …

This paper presents the attitude control design of satellite launch vehicle based on the direct
adaptive generalized dynamic inversion approach. The proposed adaptive generalized …

In this paper, we designa robust Successive Generalised Dynamic Inversion (SGDI) flight
control system for high-performance trajectory tracking of target sun-synchronous orbit …

This paper investigates adaptive flight control design strategies which are robust to a wide
range of both parametric and non-parametric uncertainties for a highly non-linear, time …

This article describes the development of a trajectory planning system which controls the
movement of a tele-commanded mobile robot through machine vision techniques and fuzzy …

This paper presents a methodology based on Differential Evolution (DE) algorithm to
perform trajectory optimization for generating reference trajectory of a four-stage Satellite …