EUCASS book series - Advances in AeroSpace Sciences

EDPS Account

Progress in Flight Dynamics, Guidance…

Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection, and Avionics – Volume 6

St. Petersburg, Russian, July 4-8, 2011
C. Vallet, D. Choukroun, C. Philippe, G. Balas, A. Nebylov and O. Yanova (Eds.)

ISBN: 978-2-7598-0878-6

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Handling qualities

Open Access

Theoretical and experimental methods to select aircraft handling qualities p. 3

L. E. Zaichik, Y. P. Yashin, V. S. Perebatov and P. A. Desyatnik

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306003

Open Access

New aircraft configurations handling qualities studies based on the aerodynamic invariant concept p. 17

J. Bazile

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306017

Navigation and estimation

Open Access

Real-time estimation of projectile roll angle using magnetometers: in-lab experimental validation p. 35

S. Changey, E. Pecheur, P. Wey and E. Sommer

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306035

Open Access

Using distributed magnetometry in navigation of heavy launchers and space vehicles p. 45

N. Praly, P.-J. Bristeau, J. Laurent-Varin and N. Petit

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306045

Open Access

Attitude estimation of the Delfi-n3Xt satellite p. 55

D. Choukroun, A. Maas and J. M. Kuiper

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306055

Open Access

Integrated communications and optical navigation system p. 81

J. Mueller, G. Pajer and M. Paluszek

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/20130681

Open Access

Planetary rover navigation: improving visual odometry via additional images and multisensor fusion p. 97

G. Casalino, E. Zereik, E. Simetti, A. Turetta, S. Torelli and A. Sperindé

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/20130697

Guidance and control

Open Access

Mission analysis and guidance, navigation, and control design for rendezvous and docking phase of advanced reentry vehicle mission p. 123

L. Strippoli, P. Colmenarejo and H. Strauch

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306123

Open Access

Model predictive control application to spacecraft rendezvous in mars sample return scenario p. 137

M. Saponara, V. Barrena, A. Bemporad, E. N. Hartley, J. Maciejowski, A. Richards, A. Tramutola and P. Trodden

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306137

Open Access

A practical receding horizon control framework for path planning and control of autonomous vtol vehicles p. 159

C. Liu and W.-H. Chen

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306159

Open Access

Aircraft pitch attitude adaptive control via singular perturbation technique p. 175

V. D. Yurkevich

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306175

Open Access

Attitude control system of the Delfi-n3Xt satellite p. 189

J. Reijneveld and D. Choukroun

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306189

Open Access

Vega roll and attitude control system algorithms trade-off study p. 209

N. Paulino, G. Cuciniello, I. Cruciani, F. Corraro, D. Spallotta and F. Nebula

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306209

Fault detection and control

Open Access

The challenge of advanced model-based fdir techniques for aerospace systems: the 2011 situation p. 231

A. Zolghadri

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306231

Open Access

A high-fidelity airbus benchmark for system fault detection and isolation and flight control law clearance p. 249

Ph. Goupil and G. Puyou

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306249

Open Access

Optimization-based tuning of LPV fault detection filters for civil transport aircraft p. 263

D. Ossmann and A. Varga

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306263

Open Access

A decentralized fault detection and isolation scheme for spacecraft: bridging the gap between model-based fault detection and isolation research and practice p. 281

S. Indra, L. Travé-Massuyès and E. Chanthery

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306281

Open Access

Model-based fault detection and identification with online aerodynamic model structure selection p. 299

T. Lombaerts

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306299

Open Access

Fault detection and isolation of aircraft air data/inertial system p. 317

D. Berdjag, J. Cieslak and A. Zolghadri

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306317

Open Access

A benchmark for fault tolerant flight control evaluation p. 333

H. Smaili, J. Breeman, T. Lombaerts and O. Stroosma

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306333

Open Access

Flight dynamics analysis and control of transport aircraft subject to failure p. 347

O. Daşkɪran and M. Ş. Kavsaoğlu

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306347

Open Access

Tuning and comparing fault diagnosis methods for aeronautical systems via kriging-based optimization p. 363

J. Marzat, H. Piet-Lahanier, F. Damongeot and E. Walter

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306363

Open Access

Nonlinear observer techniques for oscillatory failure case detection p. 375

D. Efimov and A. Zolghadri

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306375

Open Access

Improving fault detection by extended kalman filter adjustment for oscillatory failure case in aircrafts p. 393

D. Efimov, A. Zolghadri and P. Simon

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306393

Open Access

Guaranteed robust fault detection and isolation techniques for small satellites p. 407

L. Valavani and N. Tantouris

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306407

Open Access

A model-based solution for fault diagnosis of thruster faults: application to the rendezvous phase of the mars sample return mission p. 423

D. Henry, E. Bornschlegl, X. Olive and C. Charbonnel

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306423

Open Access

Reliable amplitude and frequency estimation for biased and noisy signals − Application to oscillatory failures detection p. 443

T. Raїssi, D. Efimov and A. Zolghadri

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306443

Avionics

Open Access

A verification and validation process for model-driven engineering p. 455

R. Delmas, A. F. Pires and T. Polacsek

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306455

Open Access

Program compaction for real-time applications p. 469

A. Shalimov and R. Smeliansky

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306469

Open Access

Simulation modeling based method for choosing an effective set of fault tolerance mechanisms for real-time avionics systems p. 487

A. G. Bakhmurov, V. V. Balashov, A. B. Glonina, V. N. Pashkov, R. L. Smeliansky and D. Yu. Volkanov

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306487

Open Access

Analysis of real-time networks with monte carlo methods p. 501

C. Mauclair and G. Durrieu

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306501

Launchers trajectory optimization

Open Access

Multipayload injection conception p. 517

G. Martens, O. Lukyanovych and I. Filippenko

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306517

Open Access

Trajectory generation in a three-dimensional flight plan with obstacle avoidance for an airborne launch craft p. 531

S. Dicheva and Ya. Bestaoui

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306531

Open Access

Satellite launcher pointing for orbit injection with uncontrolled solid-propellant last stage p. 545

A. de Lima Nepomuceno and W. de Castro Leite Filho

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306545

Open Access

The through optimization of fail-safe branched injection trajectories of launch vehicles in view of aerodynamic load constraints on the basis of the maximum principle p. 569

A. S. Filatyev and O. V. Yanova

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306569

Flexible aircraft control

Open Access

ACFA 2020 − An FP7 project on active control of flexible fuel efficient aircraft configurations p. 585

R. Maier

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306585

Open Access

Configuration selection for a 450-passenger ultraefficient 2020 aircraft p. 601

D. Paulus, T. Salmon, B. Mohr, C. Roessler, Ӧ. Petersson, F. Stroscher, H. Baier and M. Hornung

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306601

Open Access

Influencing the aerodynamics of the ACFA2020 aircraft with flap and trailing edge device oscillations p. 619

M. Meyer and Ch. Breitsamter

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306619

Open Access

Reduced order model of a blended wing body aircraft configuration p. 635

F. Stroscher, Z. Sika and O. Petersson

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306635

Open Access

Fuel management system for cruise performance optimization on a large blended wing body airliner p. 651

A. Wildschek, F. Stroscher, T. Haniš and T. Belschner

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306651

Open Access

Low order H_∞ optimal control for ACFA blended wing body aircraft p. 671

T. Haniš, V. Kucera and M. Hromčík

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306671

Open Access

An ℋ_∞ full information approach for the feedforward controller design of a large blended wing body flexible aircraft p. 685

C. Westermayer, A. Schirrer, M. Hemedi and M. Kozek

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306685

Open Access

L_∞-Optimal feedforward gust load alleviation design for a large blended wing body airliner p. 707

A. Wildschek, T. Haniš and F. Stroscher

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306707

Open Access

A linear parameter-varying multiobjective control law design based on youla parametrization for a flexible blended wing body aircraft p. 729

F. Demourant and G. Ferreres

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306729

Open Access

Robust lateral blended-wing-body aircraft feedback control design using a parameterized LFR model and DGK-iteration p. 749

A. Schirrer, C. Westermayer, M. Hemedi and M. Kozek

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306749

Open Access

Delay-based signal shapers and acfa 2020 blended wing body flight control system p. 767

V. Kucera and M. Hromčík

Published online: 02 December 2013

DOI: https://doi.org/10.1051/eucass/201306767