most citedOnboard Multivariable Controller Design for a Small Scale Helicopter Using Coefficient Diagram Method

11 citations · 37 across the 11 of their papers we have counts for

collaborators

11 papers

eess.SY2016

System Identification of NN-based Model Reference Control of RUAV during Hover

Bhaskar Prasad Rimal, Idris E. Putro, Agus Budiyono +2

UAV control system is a huge and complex system, and to design and test a UAV control system is time-cost and money-cost. This paper considered the simulation of identification of…

cs.NE2008★ 2 cited

Structural Damage Detection Using Randomized Trained Neural Networks

Ismoyo Haryanto, Joga Dharma Setiawan, Agus Budiyono

A computationally method on damage detection problems in structures was conducted using neural networks. The problem that is considered in this works consists of estimating the exi…

cs.RO2008

An Algebraic Approach for the MIMO Control of Small Scale Helicopter

A. Budiyono, T. Sudiyanto

The control of small-scale helicopter is a MIMO problem. To use of classical control approach to formally solve a MIMO problem, one needs to come up with multidimensional Root Locu…

cs.RO2008★ 10 cited

Linear Parameter Varying Model Identification for Control of Rotorcraft-based UAV

Agus Budiyono, H. Y Sutarto

A rotorcraft-based unmanned aerial vehicle exhibits more complex properties compared to its full-size counterparts due to its increased sensitivity to control inputs and disturbanc…

cs.RO2008★ 4 cited

Design, Development and Testing of Underwater Vehicles: ITB Experience

Muljowidodo, Said D. Jenie, Agus Budiyono +1

The last decade has witnessed increasing worldwide interest in the research of underwater robotics with particular focus on the area of autonomous underwater vehicles (AUVs). The u…

cs.RO2008★ 11 cited

Onboard Multivariable Controller Design for a Small Scale Helicopter Using Coefficient Diagram Method

A. Budiyono

A mini scale helicopter exhibits not only increased sensitivity to control inputs and disturbances, but also higher bandwidth of its dynamics. These properties make model helicopte…