Repository Aeronautics Avionics

Flight test verification of Hardware in the Loop simulations of the PZL-130 Orlik aircraft stabilization system that uses trim tabs in the lateral channel

ALBERT ZAJDEL; MICHAŁ WELCER; CEZARY SZCZEPAŃSKI; MARIUSZ KRAWCZYK

DOI Number: 10.13009/EUCASS2023-088

A Dual-Based Linear Programming formulation of Optimal Control: Fuel-Optimal Rendezvous Guidance and Boresight Pointing Applications

SERGIO CUEVAS DEL VALLE; PABLO SOLANO-LÓPEZ; HODEI URRUTXUA

DOI Number: 10.13009/EUCASS2023-057

Embedding Pontryagin’s Principle in Neural Networks for Optimal Asteroid Landing

SERGIO CUEVAS DEL VALLE; PABLO SOLANO-LÓPEZ; HODEI URRUTXUA

DOI Number: 10.13009/EUCASS2023-056

6-DOF orbit-attitude stabilization around an asteroid by using performance based intermittent event-triggered control

HONGYI XIE; FRANCO BERNELLI-ZAZZERA

DOI Number: 10.13009/EUCASS2023-027

Dynamic Simulation, Flight Control and Guidance Synthesis for Fixed-Wing UAV Swarms

CARLO E.D. RIBOLDI; MARCO TOMASONI

DOI Number: 10.13009/EUCASS2023-026

Development of a Modular Half-Duplex Frequency-Agile X-Band Transceiver for CubeSats and Robotic Spacecraft

ROBIN BONNY; MARTIN SIMIK; JULIETTE CHALLOT; HANNES BARTLE

DOI Number: 10.13009/EUCASS2023-020

AIRPLANE GROUND TESTS WITH ROTATING FORCE SIMULATION

Regina V. Leonteva

DOI Number: N/A

Conference number: IFASD-2015-158

STATE OF THE ART OF GVT TECHNOLOGY IN RUSSIA AND POSSIBLE DIRECTIONS TO INCREASE ACCURACY AND RELIABILITY

Petr G. Karkle, Michail A. Pronin, Michail M. Bogatyrev, Gleb V. Liseykin, Klaas Dijkstra

DOI Number: N/A

Conference number: IFASD-2015-140

THE USE OF DYNAMIC STRAIN SENSORS AND MEASUREMENTS ON THE GROUND VIBRATION TESTING OF AN F-16 AIRCRAFT

Fabio L. M. dos Santos, Bart Peeters, Jan Debille, Carmine Salzano, Luiz Carlos, S. Goes, Wim Desmet

DOI Number: N/A

Conference number: IFASD-2015-122

NONLINEAR GROUND VIBRATION IDENTIFICATION OF AN F-16 AIRCRAFT PART I: FAST NONPARAMETRIC ANALYSIS OF DISTORTIONS IN FRF MEASUREMENTS

M. Vaes, J. Schoukens, Y. Rolain, B. Peeters, J. Debille, T. Dossogne3, J.P. Noël, C. Grappasonni, G. Kerschen

DOI Number: N/A

Conference number: IFASD-2015-101

AN EFFICIENT APPROACH FOR IN-OPERATION MODAL ANALYSIS OF FLUTTER FLIGHT TESTS

B. Jacquier, P. Vacher, S. Leroy, D. Walker

DOI Number: N/A

Conference number: IFASD-2015-095

NONLINEAR GROUND VIBRATION IDENTIFICATION OF AN F-16 AIRCRAFT PART II: UNDERSTANDING NONLINEAR BEHAVIOUR IN AEROSPACE STRUCTURES USING SINE-SWEEP TESTING

Dossogne, J.P. Noël, C. Grappasonni, G. Kerschen, B. Peeters, J. Debille, M. Vaes, J. Schoukens

DOI Number: N/A

Conference number: IFASD-2015-035

AIRBUS A320 NEO GVT AND FEM UPDATING STATE-OF-THE-ART TECHNIQUES TO PERFORM AN INDUSTRIAL VIBRATION TEST CAMPAIGN AND A RAPID PROCESS TO UPDATE RENEWED FEM FOR CLEARANCE OF FIRST FLIGHT TEST

C. Stephan , T-P Vo-Hoang , S. Giclais , Y. Govers , P. Lubrina , M. Boeswald , A. Laporte

DOI Number: N/A

Conference number: IFASD-2015-024

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Results

Flight test verification of Hardware in the Loop simulations of the PZL-130 Orlik aircraft stabilization system that uses trim tabs in the lateral channel

A Dual-Based Linear Programming formulation of Optimal Control: Fuel-Optimal Rendezvous Guidance and Boresight Pointing Applications

Embedding Pontryagin’s Principle in Neural Networks for Optimal Asteroid Landing

6-DOF orbit-attitude stabilization around an asteroid by using performance based intermittent event-triggered control

Dynamic Simulation, Flight Control and Guidance Synthesis for Fixed-Wing UAV Swarms

Development of a Modular Half-Duplex Frequency-Agile X-Band Transceiver for CubeSats and Robotic Spacecraft

AIRPLANE GROUND TESTS WITH ROTATING FORCE SIMULATION

STATE OF THE ART OF GVT TECHNOLOGY IN RUSSIA AND POSSIBLE DIRECTIONS TO INCREASE ACCURACY AND RELIABILITY

NONLINEAR GROUND VIBRATION IDENTIFICATION OF AN F-16 AIRCRAFT PART I: FAST NONPARAMETRIC ANALYSIS OF DISTORTIONS IN FRF MEASUREMENTS

NONLINEAR GROUND VIBRATION IDENTIFICATION OF AN F-16 AIRCRAFT PART II: UNDERSTANDING NONLINEAR BEHAVIOUR IN AEROSPACE STRUCTURES USING SINE-SWEEP TESTING