Incremental Nonlinear flight Control supplemented with Envelope ProtecTION techniques

Informazioni relative al progetto

INCEPTION

ID dell’accordo di sovvenzione: 723515

DOI

10.3030/723515

Progetto chiuso

Data della firma CE 21 Marzo 2017

Data di avvio 1 Giugno 2017

Data di completamento 30 Novembre 2020

Finanziato da

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Costo totale

€ 2 386 456,25

Contributo UE

€ 2 386 455,75

Coordinato da

TECHNISCHE UNIVERSITAET MUENCHEN
Germany

CORDIS fornisce collegamenti ai risultati finali pubblici e alle pubblicazioni dei progetti ORIZZONTE.

I link ai risultati e alle pubblicazioni dei progetti del 7° PQ, così come i link ad alcuni tipi di risultati specifici come dataset e software, sono recuperati dinamicamente da .OpenAIRE .

Risultati finali

Documents, reports (11)

Unmanned Flight Testing Report

Deliverable 5.5 will present results of validation tests under realistic conditions executed on during the flight of UAV platform in a controlled area. In particular, this document will contain the legal authorisations, test plan, detailed test procedures, brief description of logistics activities, description of final implementaion actions specific to UAV platforms and report from flights execution.

Benchmark Requirements & Perform. Metrics Report

Deliverable 2.5 will provide the benchmark requirements in terms of performance and the corresponding performance metrics with different model uncertainities derived from aerodynamics, control effectiveness and sensor errors.

Project Summary

Deliverable 1.1 will present the summary of INCEPTION, describing main objectives of the project, means of goal achievement and work descriptions.

Hardware-in-the-loop Testing Report

Deliverable 5.3 will present the results and their analysis of simulations of INCEPTION system at a hardware-in-the-loop test bed. In particular, the document will contain the test plan, detailed test procedures, description of mathematical models used and report from simulations execution.

Feasibility & Performance Evaluation Report

Deliverable 6.2 will present the evaluation of autopilots and flight envelope protection and prediction strategies and examine whether they are applicable and certificable on a standard hardware used in aerospace applications. In particular, the document will present the current and future FCS hardware and software requirements for manned and unmanned aerial systems, current and future FCS certification requirements for manned and unmanned aerial systems, evaluation of algorithms implemented in INCEPTION in technical terms, evaluation of algorithms and design process with respect to the derived FCS requirements and conclusions on aerial platforms suitable for application of developed algorithms.

Flight Simulator Testing Report

Deliverable 5.4 will present results and their analysis of validation tests executed in a training flight simulator for manned aircraft. In particular, the document will contain definition of test scenarios and their conditions (i.e. flight condition, manoeuvres to be carried out, flight phase, disturbances and potential failures) and results from tests execution.

Scenario Analysis & System Requirements Report

Deliverable 2.1. will present high-level system requirements and specifications of scenarios used during INCEPTION concept validation (WP5) with description of scenarios, in which INCEPTION can be applied. In particular, this deliverable will compile: operational requirements, technical requirements, reference aircraft, reference flight manoeuvres and preliminary definition of validation tests with objectives.

Evaluation, Dissemination and Exploitation Plan [2]

This is an updated on Deliverable 6.1 which will include more detailed plans for evaluation, dissemination and mostly exploitation

Communication & Outreach Reports

Deliverable 6.3 will describe activities caried on and tolls used to promote the project and its progress during the execution such as regular updates of project website, preparation of project brochurem attending conferences and seminars.

Evaluation, Dissemination and Exploitation Plan [1]

Deliverable 6.1 will include evaluation, dissemination and exploitation plans that will be followed during the execution of the project. An analysis of possible impacts of FCS architecture on INCEPTION performance will be performed.

Final brochure for official public presentation issues

Deliverable 6.6 will present the final brochure of INCEPTION used for dissemination purposes.

Websites, patent fillings, videos etc. (1)

Website and logo

Deliverable 6.5 will present the project logo and website.

Pubblicazioni

Conference proceedings (5)

Two-layer Fault Detection for Incremental Flight Control of Fixed-wing UAV

Autori: Dmitry I. Ignatyev, Hyo-Sang Shin, Antonios Tsourdos
Pubblicato in: 2019 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED UAS), 2019, Pagina/e 227-236, ISBN 978-1-7281-6600-1
Editore: IEEE
DOI: 10.1109/reduas47371.2019.8999692

Understandings of the Incremental Backstepping Control Through Theoretical Analysis Under the Model Uncertainties

Autori: Byoung-Ju Jeon, Min-Guk Seo, Hyo-Sang Shin, Antonios Tsourdos
Pubblicato in: 2018 IEEE Conference on Control Technology and Applications (CCTA), 2018, Pagina/e 318-323, ISBN 978-1-5386-7698-1
Editore: IEEE
DOI: 10.1109/CCTA.2018.8511479

Robust Incremental Backstepping Controller for the Attitude and Airspeed Tracking of a Commercial Airplane

Autori: Nuno Miguel Guerreiro, Alexandra Moutinho
Pubblicato in: 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering (ICMAE), 2019, Pagina/e 607-611, ISBN 978-1-7281-5535-7
Editore: IEEE
DOI: 10.1109/icmae.2019.8881034

Flight Envelope Protections using Phase Plane Limits and Backstepping Control,” in

Autori: Agnes Christine Gabrys, Rasmus Steffensen, Rafael de Angelis Cordeiro, José Raul Azinheira, Alexandra Moutinho, Florian Holzapfel
Pubblicato in: Proc. of 5th CEAS Conference on Guidance, Navigation & Control (EuroGNC), 2019
Editore: EuroGNC

Cascaded Incremental Backstepping Controller for the Attitude Tracking of Fixed-Wing Aircraft

Autori: Rafael A. Cordeiro, José R. Azinheira, Alexandra Moutinho
Pubblicato in: Proc. of 5th CEAS Conference on Guidance, Navigation and Control (EuroGNC), 2019
Editore: EuroGNC

Peer reviewed articles (7)

Understandings of Classical and Incremental Backstepping Controllers with Model Uncertainties

Autori: Byoung-Ju Jeon, Min-Guk Seo, Hyo-Sang Shin, Antonios Tsourdos
Pubblicato in: IEEE Transactions on Aerospace and Electronic Systems, 2019, Pagina/e 1-1, ISSN 0018-9251
Editore: Institute of Electrical and Electronics Engineers
DOI: 10.1109/taes.2019.2952631

Closed-loop Analysis with Incremental Backstepping Controller considering Measurement Bias

Autori: Byoung-Ju Jeon, Min-Guk Seo, Hyo-Sang Shin, Antonios Tsourdos
Pubblicato in: IFAC-PapersOnLine, Numero 52/12, 2019, Pagina/e 405-410, ISSN 2405-8963
Editore: Elsevier
DOI: 10.1016/j.ifacol.2019.11.277

Addressing Actuation Redundancies in Incremental Controllers for Attitude Tracking of Fixed-Wing Aircraft

Autori: Rafael A. Cordeiro, José R. Azinheira, Alexandra Moutinho
Pubblicato in: IFAC-PapersOnLine, Numero 52/12, 2019, Pagina/e 417-422, ISSN 2405-8963
Editore: Elsevier
DOI: 10.1016/j.ifacol.2019.11.279

Two-Layer On-line Parameter Estimation for Adaptive Incremental Backstepping Flight Control for a Transport Aircraft in Uncertain Conditions

Autori: Dmitry I. Ignatyev, Hyo-Sang Shin, Antonios Tsourdos
Pubblicato in: IFAC-PapersOnLine, Numero 52/12, 2019, Pagina/e 411-416, ISSN 2405-8963
Editore: Elsevier
DOI: 10.1016/j.ifacol.2019.11.278

Integration of Phase Plane Flight Envelope Protections in Cascaded Incremental Flight Control

Autori: Agnes Christine Gabrys, Rasmus Steffensen, Rafael de Angelis Cordeiro, José Raul Azinheira, Alexandra Moutinho, Florian Holzapfel
Pubblicato in: IFAC-PapersOnLine, Numero 52/12, 2019, Pagina/e 429-435, ISSN 2405-8963
Editore: Elsevier
DOI: 10.1016/j.ifacol.2019.11.281

Understandings of incremental backstepping controller considering measurement delay with model uncertainty

Autori: Byoung-Ju Jeon, Min-Guk Seo, Hyo-Sang Shin, Antonios Tsourdos
Pubblicato in: Aerospace Science and Technology, Numero 109, 2021, Pagina/e 106408, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2020.106408

Two-layer adaptive augmentation for incremental backstepping flight control of transport aircraft in uncertain conditions

Autori: Dmitry I. Ignatyev, Hyo-Sang Shin, Antonios Tsourdos
Pubblicato in: Aerospace Science and Technology, Numero 105, 2020, Pagina/e 106051, ISSN 1270-9638
Editore: Elsevier BV
DOI: 10.1016/j.ast.2020.106051

Thesis and dissertations (1)

Incremental Backstepping Control of Fixed-Wing Commercial Aircraft under Uncertainties

Autori: Nuno Miguel Serrano Guerreiro
Pubblicato in: 2019
Editore: Instituto Superior Técnico