| Paper number |
Paper author(s) |
Paper title |
| CEAS-GNC-2019-002 |
Zeynep Unal, Gonenc Gursoy, Ilkay Yavrucuk |
Simulator Based Evaluation for Helicopter Load Factor Limit Avoidance with Concurrent Learning |
| CEAS-GNC-2019-003 |
Rasmus Steffensen, Agnes Gabrys, Florian Holzapfel |
Flight Envelope Protections Using Phase Plane Limits and Backstepping Control |
| CEAS-GNC-2019-004 |
Giacomo Gerosa, Andrea Zanoni, Simone Panza, Pierangelo Masarati, Marco Lovera |
Augmented Rotorcraft Conceptual Design Driven by Handling Qualities Requirements |
| CEAS-GNC-2019-005 |
Jana Schwithal, Nicolas Fezans, Dominik Niedermeier |
Integration of Wake Impact Alleviation Control System into Control System Architecture of Modern Fly-By-Wire Aircraft |
| CEAS-GNC-2019-006 |
Seokwon Lee, Youdan Kim |
Passivity-based Angular Rate Feedback Controller for Fin-Controlled Missiles |
| CEAS-GNC-2019-007 |
G. Bressan, D. Invernizzi, S. Panza, M. Lovera |
Attitude control of multirotor UAVs: cascade P/PID vs PI-like architecture |
| CEAS-GNC-2019-010 |
Federico Fumenti, David Seelbinder, Stephan Theil |
Application of Mean-Motion-Based Artificial Potentials for a Cluster Flight Mission Scenario |
| CEAS-GNC-2019-011 |
Stefano Silvestrini, Vincenzo Pesce, Michèle Lavagna |
Distributed Autonomous Guidance, Navigation and Control loop for Formation Flying Spacecraft Reconfiguration |
| CEAS-GNC-2019-012 |
Priya G. Nair, Ashok Joshi |
A Modified Re-entry Trajectory Planning Approach and Comparison with EAGLE Method |
| CEAS-GNC-2019-013 |
P. Simplício, A. Marcos, S. Bennani |
A Reusable Launcher Benchmark with Advanced Recovery Guidance |
| CEAS-GNC-2019-014 |
Marius Klein, Andreas Klos, Wolfram Schiffmann |
Glide path generation with regard to wind misestimations |
| CEAS-GNC-2019-015 |
Michael Hardt, Robert Höpler |
Generating Aircraft Trajectories encoded with the Aircraft Intent Description Language using the Modeling Language Modelica |
| CEAS-GNC-2019-016 |
Nicolai Voget, Johannes Krimphove, Dieter Moormann |
Flight Planning Using Time Annotated B-Splines for Safe Airspace Integration |
| CEAS-GNC-2019-017 |
Seyed M. Malaek, Sina Moradi |
Trajectory Optimization of Microgravity Atmospheric Flights Based on a Hybrid Heuristic Algorithm |
| CEAS-GNC-2019-018 |
Luca d'Avico, Mara Tanelli, Sergio M. Savaresi |
Dynamic analysis of tire consumption in aircraft anti-skid braking |
| CEAS-GNC-2019-019 |
Ahmed Khalil, Nicolas Fezans |
A Multi-Channel H∞ Preview Control Approach to Load Alleviation Function Design |
| CEAS-GNC-2019-020 |
Özge Süelözgen |
Advanced Aeroelastic Robust Stability Analysis with Structural Uncertainties |
| CEAS-GNC-2019-021 |
Julian Theis, Frank Thielecke |
A Generic Rendezvous Control Solution for Automatic Landing of Unmanned Aircraft |
| CEAS-GNC-2019-022 |
Ahmed Aly Kamel |
Improved Instrument Misalignment Equations for Image Navigation and Registration (INR) |
| CEAS-GNC-2019-023 |
Ahmed Aly Kamel |
Improved Image Navigation and Registration (INR) Algorithms |
| CEAS-GNC-2019-024 |
C. Nainer, H. Garnier, M. Gilson, H. Evain, C. Pittet |
In-Flight Inertia Matrix Estimation of a Gyroless Satellite |
| CEAS-GNC-2019-025 |
Daniel Choukroun, Uri Tamir |
A Novel Multiplicative Quaternion Filter |
| CEAS-GNC-2019-027 |
Alexander Köthe, Robert Luckner |
Applying Eigenstructure Assignment to Inner-Loop Flight Control Laws for a Multibody Aircraft |
| CEAS-GNC-2019-028 |
Alexander Köthe, Robert Luckner |
Outer-Loop Control Law Design with Control Allocation for a Multibody Aircraft |
| CEAS-GNC-2019-029 |
Stephen C. Hungs, Erik-Jan van Kampen |
Finding all trimmable flight conditions of an over-actuated aircraft using interval analysis |
| CEAS-GNC-2019-030 |
Rob Stolk, Coen de Visser |
Minimum drag control allocation for the Innovative Control Effector aircraft |
| CEAS-GNC-2019-031 |
Patrick Piprek, Sébastien Gros, Florian Holzapfel |
A Distributed Robust Optimal Control Framework Based on Polynomial Chaos |
| CEAS-GNC-2019-032 |
Christian Weiser, Daniel Ossmann, Richard Kuchar, Gertjan Looye |
Design and Verification of a Linear Parameter Varying Control Law for a Transport Aircraft |
| CEAS-GNC-2019-033 |
Donghyeok Hwang, Min-Jea Tahk |
Optimal guaranteed cost sliding mode control for a missile with unmatched uncertainties |
| CEAS-GNC-2019-034 |
Andrea Iannelli, Mark Lowenberg, Andrés Marcos |
An extension of the structured singular value to nonlinear systems with application to robust flutter analysis |
| CEAS-GNC-2019-035 |
Gustav Öman Lundin, Philippe Mouyon, Augustin Manecy |
Experimental study of an attitude estimator with measurement disturbance rejection |
| CEAS-GNC-2019-036 |
Johann Meyer, Kreelan Padayachee, Benjamin A. Broughton |
A Robust Complementary Filter Approach for Attitude Estimation of Unmanned Aerial Vehicles using AHRS |
| CEAS-GNC-2019-037 |
Alberto Brandl, Angelo Lerro, Manuela Battipede, Piero Gili |
Air Data Virtual Sensor: a Data-Driven Approach to Identify Flight Test Data Suitable for the Learning Process |
| CEAS-GNC-2019-038 |
Meiliwen Wu, Marco Lovera |
Time-domain vs frequency-domain identification for a small-scale helicopter |
| CEAS-GNC-2019-039 |
Su Jan Kieran Kersbergen, Sihao Sun, Coen de Visser |
Qualitative Loss-Of-Control of Quadrotors |
| CEAS-GNC-2019-040 |
Marco Maccotta, Marco Lovera |
Reconfigurability analysis of multirotor UAVs |
| CEAS-GNC-2019-041 |
Angelo Zangarini, Davide Invernizzi, Pietro Panizza, Marco Lovera |
Closed-loop MIMO data-driven attitude control design for a multirotor UAV |
| CEAS-GNC-2019-042 |
P. Giuri, A. Marini Cossetti, M. Giurato, D. Invernizzi, M. Lovera |
Air-to-air automatic landing for multirotor UAVs |
| CEAS-GNC-2019-043 |
Kaustubh Sridhar, Srikant Sukumar |
Finite-time, Event-triggered Tracking Control of Quadrotors |
| CEAS-GNC-2019-044 |
Heekun Roh, Young-Jae Oh, Min-Jea Tahk, Chang-Hun Lee |
Fast Trajectory Optimization Using Sequential Convex Method for Guided Missiles |
| CEAS-GNC-2019-045 |
Michael Proff, Spilios Theodoulis, |
Study of Impact Point Prediction Methods for Zero-Effort-Miss Guidance: Application to a 155mm Spin-Stabilized Guided Projectile |
| CEAS-GNC-2019-046 |
Jaeho Lee, Seokwon Lee, Youdan Kim |
Nonlinear Disturbance Observer-Based Attitude Controller for Exoatmospheric DACS Type Missile Considering Seeker's Field-of-View Limit |
| CEAS-GNC-2019-047 |
Ozgun Dulgar, Rustu Berk Gezer, Ali Turker Kutay |
Kalman Filter Based Altitude Control Approach for Sea Skimming Cruise Missiles with Sea Wave Adaptation |
| CEAS-GNC-2019-048 |
Rafał Ożóg, Robert Głębocki, Mariusz Jacewicz |
Side thrusters firing logic for artillery rocket |
| CEAS-GNC-2019-049 |
Magalhães Oliveira, Hans Krüger, Stephan Theil |
Feature-based Optical Navigation for Lunar Landings |
| CEAS-GNC-2019-050 |
A. W. I. Mohamed, C. M. Saaj, A. Seddaoui, S. Eckersley |
Controlling a Non-Linear Space Robot using Linear Controllers |
| CEAS-GNC-2019-051 |
James D. Biggs, Hugo Fournier, Simone Ceccherini, Francesco Topputo |
Optimal de-tumbling of spacecraft with four thrusters |
| CEAS-GNC-2019-052 |
Cristiano Contini, Camilla Colombo |
Attitude and Orbital Dynamics Coupled Simulator For High Area-to-Mass Ratio Satellites |
| CEAS-GNC-2019-054 |
Barak Or, Joseph Z. Ben-Asher, Isaac Yaesh |
Imperfect Information Game for a Simple Pursuit-Evasion Problem |
| CEAS-GNC-2019-055 |
Fabio Curti, Marcello Romano |
Minimum-Time Control of Linear Systems between Arbitrary States |
| CEAS-GNC-2019-056 |
K. C. Tejaswi, Sukumar Srikant |
Backstepping control for state constrained systems |
| CEAS-GNC-2019-057 |
Mathieu Petit, Camilla Colombo |
Optimal Deflection of Resonant Near-Earth Objects Using the B-Plane |
| CEAS-GNC-2019-058 |
Giovanni Purpura, Pierluigi Di Lizia |
An autonomous GNC strategy for asteroid impactor missions |
| CEAS-GNC-2019-059 |
Ricardo García-Pelayo, Juan Luis Gonzalo |
Probability of collision between a rectangular cuboid and small debris |
| CEAS-GNC-2019-060 |
Himani Sinhmar, Sukumar Srikant |
Distributed model independent algorithm for spacecraft synchronization under relative measurement bias |
| CEAS-GNC-2019-061 |
Jianqiao Zhang, James D. Biggs, Zhaowei Sun |
Relative orbit-attitude tracking for spacecraft using adaptive fast terminal sliding mode control |
| CEAS-GNC-2019-062 |
Hongyang Dong, Qinglei Hu, Maruthi R. Akella |
Composite Adaptive Control for Robot Manipulator Systems |
| CEAS-GNC-2019-063 |
Daniel Ossmann, Charles Poussot-Vassal |
Design and Assessment of a Two Degree of Freedom Gust Load Alleviation System |
| CEAS-GNC-2019-064 |
Karl Frederik Prochazka, Tobias Ritz, Hugo Eduardo |
Over-Actuation Analysis and Fault-Tolerant Control of a Hybrid Unmanned Aerial Vehicle |
| CEAS-GNC-2019-065 |
Stéphane Delannoy |
Airbus Generic Control Laws |
| CEAS-GNC-2019-066 |
Rafael A. Cordeiro, José R. Azinheira, Alexandra Moutinho |
Cascaded Incremental Backstepping Controller for the Attitude Tracking of Fixed-Wing Aircraft |
| CEAS-GNC-2019-067 |
A. Efremov, M. Tiagilk, I. Irgaleev |
The Potential of the Display with Path Motion Prediction and Preview of the Planned Trajectory |
| CEAS-GNC-2019-068 |
Antoine Monneau, Nacer K M'Sirdi, Sebastien Mavromatis, Guillaume Varra, Marc Salesse, Jean Sequeira |
Adaptive Prediction for Ship Motion in Rotorcraft Maritime Operations |
| CEAS-GNC-2019-069 |
Boguslaw Dolega, Piotr Gomolka, Zbigniew Gomolka, Damian Kordos |
Cognitive Research on Pilot's Eye Attention During Flight Simulator Tests |
| CEAS-GNC-2019-070 |
Nicolas Sedlmair, Julian Theis, Frank Thielecke |
Design and Experimental Validation of UAV Control Laws - 3D Spline-Path-Following and Easy-Handling Remote Control |
| CEAS-GNC-2019-071 |
I. Barz, P. Hartmann, D. Moormann |
Near-Term Flight Path Adaption for Tilt-Wing Aircraft Obstacle Avoidance |
| CEAS-GNC-2019-072 |
Andreas Klos, Jörg Lenhardt, Marius Klein, Wolfram Schiffmann |
Multi-Modal Image Processing Pipeline for a Reliable Emergency Landing Field Identification |
