Longitudinal dynamic system modeling of a fixed-wing UAV towards autonomous flight control system development: A case study of BPPT wulung UAV platform

Triputra, Fadjar Rahino; Trilaksono, Bambang Riyanto; Sasongko, Rianto Adhy; Dahsyat, Mohamad

doi:10.1109/icsengt.2012.6339294

Cited by 19 publications

(14 citation statements)

References 4 publications

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“…The aircraft considered and selected have wingspans ranging from 2.4 to 5.8 meters and show only slight variations in their geometry. For one of them [14], the model has been made with three different techniques (analytical, grey-box method and black box method), with remarkable differences in its parameters among these techniques. For another two models [15,16], only three of the four considered variables agree.…”

Section: A Models From Research Papersmentioning

confidence: 99%

On the Tradeoff Between Electrical Power Consumption and Flight Performance in Fixed-Wing UAV Autopilots

Bertrán

Sànchez-Cerdà

2016

IEEE Trans. Veh. Technol.

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-This paper sets out a study of the autopilot design for fixed wing UAVs taking into account the aircraft stability, and also the power consumption as a function of the selected control strategy. To provide some generality to the outcomes of this study, construction of a reference small-UAV model, based on averaging the main aircraft defining parameters, is proposed. Using such a reference model of small, fixed-wing UAVs, different control strategies are assessed especially with a view towards enlarging the controllers' sampling time. A beneficial consequence of this sample time enlargement is that the clock rate of the UAV autopilots may be proportionally reduced. This reduction in turn leads directly to decreased electrical power consumption. Such energy saving becomes proportionally relevant as the size and power of the UAV decreases, with benefits of lengthening battery life and, therefore, the flight endurance. Additionally, through the averaged model, derived from both published data and computations made from actual data captured from real UAVs, it is shown that behavior predictions beyond that of any particular UAV model may be extrapolated.

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Section: A Models From Research Papersmentioning

confidence: 99%

On the Tradeoff Between Electrical Power Consumption and Flight Performance in Fixed-Wing UAV Autopilots

Bertrán

Sànchez-Cerdà

2016

IEEE Trans. Veh. Technol.

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“…which, when used in conjunction with T c and T b from equations (14) and (16), generates the required canonical form. 1) Canonical Form for Sliding Mode Control Design: Let (A, B,C) be a linear system with p > m and rank (CB) = m. Then a change of coordinates exists so that the system triple with respect to the new coordinates has the following structure:…”

Section: A Switching Function Designmentioning

confidence: 99%

Sliding mode control: a tutorial

Spurgeon

2014

2014 European Control Conference (ECC)

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“…An adaptive Backstepping approach to obtain directional control of a commercial fixedwing UAV in presence of unknown crosswind is developed in [1]. [13] of a fixed-wing UAV. [8] presents an autonomous visionbased net-recovery system for a small fixed wing UAV, and avionics were developed using several sensors, integrated with a flight control system and vision system.…”

Section: Introductionmentioning

confidence: 99%

Mini airplane: Design, aerodynamic modeling and stability

Guerrero¹,

Martinez²,

García³

et al. 2014

2014 11th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)

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This paper presents the development of a mini airplane UAV, focusing on the aerodynamic design, modeling and stability. Mathematical model of the vehicle is obtained using the Euler-Lagrange formulation and includes aerodynamic parameters of the design. For the stability, a classic control law is proposed taking in account the aerodynamic parameters and the sensors bandwidth implemented in the aircraft. Simulation results are shown for the closed-loop system of the vehicle. Finally, aerodynamic design and avionics are based on flying and handling qualities for having a mini airplane that performs a reliable and stable flight.

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Longitudinal dynamic system modeling of a fixed-wing UAV towards autonomous flight control system development: A case study of BPPT wulung UAV platform

Cited by 19 publications

References 4 publications

On the Tradeoff Between Electrical Power Consumption and Flight Performance in Fixed-Wing UAV Autopilots

On the Tradeoff Between Electrical Power Consumption and Flight Performance in Fixed-Wing UAV Autopilots

Sliding mode control: a tutorial

Mini airplane: Design, aerodynamic modeling and stability

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