| Paper Code | Title | Authors |
|---|
| Mo-A02-TO/1 | Bifurcation Analysis of Flight Control Systems | Thomas Suba, Kwatny Harry G., Chang Bor-Chin |
| Mo-A02-TO/2 | Coefficient Diagram Method in MIMO Application: An Aerospace Case Study | Manabe Shunji |
| Mo-A02-TO/3 | Comparison of Linear Dynamic Models for Air Traffic Management | Sridhar Banavar, Menon P.K. |
| Mo-A02-TO/4 | Design of Longitudinal Control System for a Nonlinear F-16 Fighter using MSS Method | Wong Y. K., Fung Eric H. K., Liu Hugh H. T., Li Y.C. |
| Mo-A02-TO/5 | Robust Global Exponential Stabilization of an Underactuated Airship | Yamada Manabu, Tomizuka Masayoshi |
| Mo-A02-TO/6 | Stabilization of a PVTOL Aircraft with Delay in the Input | Francisco Rogelio, Mazenc Frédéric, Mondié Sabine |
| Mo-E02-TO/1 | Flexible Aerospace Vehicles Simulation and Nonlinear Control Synthesis | Nebylov Alexander, Brodsky Sergey, Panferov Alexander |
| Mo-E02-TO/2 | Nonlinear Dynamics and Control of a New Hydrazine Pump Generation | Vannier JC, Arzandé A., Siguerdidjane Houria, Vidal P., Dugué F. |
| Mo-E02-TO/3 | Nonlinear H∞ for Spacecraft Attitude Control | Shou Ho-Nien, Jan Ying-Wen |
| Mo-E02-TO/4 | Robust Nonlinear Gyromoment Control of Agile Remote Sensing Spacecraft | Somov Yevgeny, Butyrin Sergey, Somov Sergey, Matrosov Vladimir, Anshakov Gennady |
| Mo-E02-TO/5 | Stability Margin Analysis in Multiobjective Design: Application to an Aerospace Launcher | Abbas-Turki Mohamed, Duc Gilles, Clement Benoît |
| Mo-E02-TO/6 | The design method of robust control by flexible spacecraft | Rutkovsky Vladislav, Zemlyakov S. D., Sukhanov V. M., Glumov V. M. |
| Th-A18-TO/1 | Cable Assisted Rendezvous for Aircraft with Surface Locations | Sgarioto Daniel, Trivailo Pavel |
| Th-A18-TO/2 | Computation of worst-case pilot inputs for clearance of flight control laws | Menon Prathyush, Bates Declan G., Postlethwaite Ian |
| Th-A18-TO/3 | Controller gains adjustment for closed-loop modal requirements | Delmond Fabien, Cumer Christelle, Alazard Daniel |
| Th-A18-TO/4 | Hybrid Optimisation schemes for the clearance of flight control laws | Menon Prathyush, Bates Declan G., Postlethwaite Ian |
| Th-A18-TO/5 | Nonlinear Dynamics and Robust Control of a Gyroplane Rotor | Somov Yevgeny, Polyntsev Oleg |
| Th-A18-TO/6 | Mixed H2/Hinfinity Sub-Optimization Approach For Integrated Aircraft/Controller Design | Liao Fang, Lum Kai Yew, Wang Jian Liang |
| Th-E18-TO/1 | Awiator's Design of Multi-Objectives Control Laws | Jeanneau Matthieu, Lamolie Jérôme, Puyou Guilhem, Aversa Nicky |
| Th-E18-TO/2 | Adaptive Reconfigurable Flight Control System Using Multiple Model Mode Switching | Kim Youdan, Jung Bokyung, Jeong Seong-Kyun, Lee Dong-Hyun |
| Th-E18-TO/3 | Observer-based control of a PVTOL aircraft | Sánchez Anand, Fantoni Isabelle, Lozano Rogelio, De León Morales Jesús |
| Th-E18-TO/4 | Low order Control Augmentation System Designs for the Helicopter UH-60 | Prempain Emmanuel, Dzeukou Marc Olivier |
| Th-E18-TO/5 | Longitudinal Axis Flight Control Law Design by Adaptive Backstepping | Ju Hann-Shing, Tsai Ching-Chih |
| Th-E18-TO/6 | QFT for the Design of an Aircraft Flight Control | Santander Alexander, Aranda Joaquin |
| Th-M01-PL/1 | The Mars Exploration Rovers: Hitting the Road on Mars | Cox Nagin |
| Th-M01-TO/1 | The CASSINI / HUYGENS Space Mission to Explore the Saturnian System | Schilling Klaus |
| Th-M01-TO/2 | Optimal Discrete-Time Magnetic Attitude Control of Satellites | Lovera Marco, Varga Andras |
| Th-M01-TO/3 | Remote Control of Target in Space using Magnetic Force | Nagai Masaki, Nakasuka Shinichi |
| Th-M01-TO/4 | Robust Control of a Spacecraft Respinup by Weak Internal Forces | Somov Yevgeny, Titov Gennady, Butyrin Sergey, Rayevsky Valentine, Kozlov Albert |
| Th-M01-TO/5 | Satellite Attitude Tracking by Quaternion-Based Backstepping | Kristiansen Raymond, Nicklasson Per Johan, Gravdahl Jan Tommy |
| Fr-A18-TO/1 | New Guidance Law and Autopilot Design for Launch Rockets | Cheng Chia-Hao, Yeh Fu-Kuang, Fu Li-Chen |
| Fr-A18-TO/2 | Attitude Control of Flexible Launch Vehicle Using Adaptive Notch Filter | Oh Choong-Seok, Bang Hyochoong |
| Fr-A18-TO/3 | LQG Controller Designs from Reduced Order Models for a Launch Vehicle | Dhabale Ashwin, Banavar Ravi, Dhekane M. V. |
| Fr-A18-TO/4 | Missile Autopilot Controlled by Aerodynamic Lift and Divert Thrusters via Second-order Sliding Mode | Shtessel Yuri, Tournes Christian, Shkolnikov Ilya |
| Fr-A18-TO/5 | Autopilot Design for Agile Missile Using LTV Control and Nonlinear Dynamic Inversion | Choi Jae Weon, Lee Ho Chul |
| Fr-A18-TO/6 | Input-Dependent Threshold Function fo an Actuator Fault Detection Filter | Rotstein Hector, Ingvalson Ryan, Keviczky Tamas, Balas Gary |
| Fr-M04-TP/1 | A new position-based method for GPS signal FDI | Castaldi Paolo, Crisci Massimo, Zanzi Matteo |
| Fr-M04-TP/2 | Antenna LQG Controllers: Properties, Limits of Performance and Tuning Procedure | Gawronski Wodek |
| Fr-M04-TP/3 | Development of MEMS angular rate sensor for high-dynamics applications | Sung Woon-Tahk, Lee Jang Gyu, Kang Taesam, Jang Hyun-Gee |
| Fr-M04-TP/4 | Multivariable closed-loop control of the reattachment length downstream of a backward-facing step | Henning Lars, King Rudibert |
| Fr-M04-TP/5 | Nonlinear Robust Performance Analysis Of An Aeroelastic System | Kim Jongrae, Bates Declan G., Postlethwaite Ian |
| Fr-M04-TP/6 | Oscillation Problem in Pitch Angle Control of Winged Body | Skrjanc Igor, Lepetić Marko, Blažič Sašo, Morita Yasuhiro |
| Fr-M04-TP/7 | Sensorimotor Convergence in Visual Navigation and Flight Control Systems | Humbert J. Sean, Murray Richard M., Dickinson Michael H. |
| Fr-M04-TP/8 | Using Delta Range on GPS Positioning, Fault Detection and Fault Exclusion | Chang Fan-Ren, Tsai Yi-Hsueh, Yang Wen-Chieh |
| Fr-M06-TP/1 | Hybrid Fault Detection and Isolation Method for UAV Inertial Sensor Redundancy Management System | Kim Youdan, Kim Hyoung Seok, Park Sang Kyun, Park Chan Gook |
| Fr-M06-TP/2 | Missile Endgame Analysis via Multiobjective Optimization | Chipperfield Andrew, Patel N., Keane A. J. |
| Fr-M06-TP/3 | Missile Guidance Design using Optimal Trajectory Shaping and Neural Network | Jan Horn-Yong, Lin Chun-Liang, Chen Kai-Ming, Lai Chi-Wen, Hwang Thong-Shing |
| Fr-M06-TP/4 | Nonlinear attitude and gyroscope's bias estimation for a VTOL UAV | Pflimlin Jean-Michel, Hamel Tarek, Souères Philippe, Metni Najib |
| Fr-M06-TP/5 | Optimal UCAV path planning under missile threats | Meerkov Semyon, Kabamba Pierre T., Zeitz III Frederick H. |
| Fr-M06-TP/6 | UAV Routing in a Stochastic, Time-Varying Environment | Frazzoli Emilio, Enright John J. |
| Fr-M07-TP/1 | Active Vibration Suppression of Flexible Spacecraft using Feed-Forward/Feedback Control Strategies | Hu Qinglei, Ma Guangfu, Liu Yaqiu |
| Fr-M07-TP/2 | Multiple Spacecraft Formation Control Using Theta-D Method | Balakrishnan Sivasubramanya, Xin Ming, Pernicka Hank |
| Fr-M07-TP/3 | Optimal Trajectory Planning of Formation Flying Spacecraft | Dumitriu Dan, Lima Pedro, Udrea Bogdan |
| Fr-M07-TP/4 | Orientation Control of an Artificial Satellite by Means of the Interval-Multiplex Approach | Shevchenko Vladimir, Lychak Mykhailo |
| Fr-M07-TP/5 | Robust Load-sharing Control of Spacecraft Formations | Garcia-Sanz Mario, Hadaegh F.Y. |
| Fr-M07-TP/6 | The LORF Orbit Equation with Full Quaternions | Andreis Davide, Canuto Enrico |
| Fr-M15-TO/1 | Online approximators for the actuators FDI of a small commercial aircraft | Paviglianiti Gaetano, Mattei Massimiliano |
| Fr-M15-TO/2 | Robust Estimation versus Optimal Estimation and their Application for Airborne Gravimetry | Kulakova Veronica I., Nebylov Alexander V., Stepanov Oleg A. |
| Fr-M15-TO/3 | Kinematics optimization for a flapping-wing micro air vehicule | Ouladsine Mustapha, Rakotomonjy Thomas, Le Moing Thiery |
| Fr-M15-TO/4 | On-Board Statistical Detection and Control of Anomalous Pilot-Aircraft Interactions | Dimogianopoulos Dimitrios, Hios John D., Fassois Spilios D. |
| Fr-M15-TO/5 | Robust Control of PVTOL Aircraft using Saturations Functions | Salazar-Cruz Sergio, Lozano Rogelio |
| Fr-M15-TO/6 | Wing-in-Ground Flight Automatic Control Systems | Nebylov Alexander, Danilov Sergey, Nebylov Vladimir, Rumyantseva Elizaveta |
