Aerobatic Aircraft Guidance Design for Air-Race Scenario

P. Promod; Atnab Maity; Haichao Hong; Matthias Bittner; Florian Holzapfel

doi:10.1109/CCTA.2019.8920721

Aerobatic Aircraft Guidance Design for Air-Race Scenario

P. Promod, Atnab Maity, Haichao Hong, Matthias Bittner, Florian Holzapfel

Chair of Flight System Dynamics

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

1 Scopus citations

Abstract

The guidance design of aerobatic aircraft in air-race is to ensure several stringent terminal conditions at the race gates as well as to satisfy bounds on control and structural load factor. Also, it should be robust in presence of uncertainties in aerodynamic parameters. All these complexities make it a challenging problem. To meet these requirements, the generalized model predictive static programming (G-MPSP) based suboptimal guidance design with hard terminal and input inequality constraints is presented in this paper. Penalty function approach is followed with the G-MPSP algorithm to ensure input constraints. To demonstrate the robustness of the proposed guidance algorithm, the simulation results are carried out considering aerodynamic parameter uncertainties.

Original language	English
Title of host publication	CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	795-800
Number of pages	6
ISBN (Electronic)	9781728127675
DOIs	https://doi.org/10.1109/CCTA.2019.8920721
State	Published - Aug 2019
Event	3rd IEEE Conference on Control Technology and Applications, CCTA 2019 - Hong Kong, China Duration: 19 Aug 2019 → 21 Aug 2019

Publication series

Name	CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications

Conference

Conference	3rd IEEE Conference on Control Technology and Applications, CCTA 2019
Country/Territory	China
City	Hong Kong
Period	19/08/19 → 21/08/19

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10.1109/CCTA.2019.8920721

Cite this

Promod, P., Maity, A., Hong, H., Bittner, M., & Holzapfel, F. (2019). Aerobatic Aircraft Guidance Design for Air-Race Scenario. In CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications (pp. 795-800). Article 8920721 (CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCTA.2019.8920721

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title = "Aerobatic Aircraft Guidance Design for Air-Race Scenario",

abstract = "The guidance design of aerobatic aircraft in air-race is to ensure several stringent terminal conditions at the race gates as well as to satisfy bounds on control and structural load factor. Also, it should be robust in presence of uncertainties in aerodynamic parameters. All these complexities make it a challenging problem. To meet these requirements, the generalized model predictive static programming (G-MPSP) based suboptimal guidance design with hard terminal and input inequality constraints is presented in this paper. Penalty function approach is followed with the G-MPSP algorithm to ensure input constraints. To demonstrate the robustness of the proposed guidance algorithm, the simulation results are carried out considering aerodynamic parameter uncertainties.",

author = "P. Promod and Atnab Maity and Haichao Hong and Matthias Bittner and Florian Holzapfel",

note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 3rd IEEE Conference on Control Technology and Applications, CCTA 2019 ; Conference date: 19-08-2019 Through 21-08-2019",

year = "2019",

month = aug,

doi = "10.1109/CCTA.2019.8920721",

language = "English",

series = "CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications",

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Promod, P, Maity, A, Hong, H, Bittner, M & Holzapfel, F 2019, Aerobatic Aircraft Guidance Design for Air-Race Scenario. in CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications., 8920721, CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications, Institute of Electrical and Electronics Engineers Inc., pp. 795-800, 3rd IEEE Conference on Control Technology and Applications, CCTA 2019, Hong Kong, China, 19/08/19. https://doi.org/10.1109/CCTA.2019.8920721

Aerobatic Aircraft Guidance Design for Air-Race Scenario. / Promod, P.; Maity, Atnab; Hong, Haichao et al.
CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications. Institute of Electrical and Electronics Engineers Inc., 2019. p. 795-800 8920721 (CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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T1 - Aerobatic Aircraft Guidance Design for Air-Race Scenario

AU - Promod, P.

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AU - Bittner, Matthias

AU - Holzapfel, Florian

PY - 2019/8

Y1 - 2019/8

N2 - The guidance design of aerobatic aircraft in air-race is to ensure several stringent terminal conditions at the race gates as well as to satisfy bounds on control and structural load factor. Also, it should be robust in presence of uncertainties in aerodynamic parameters. All these complexities make it a challenging problem. To meet these requirements, the generalized model predictive static programming (G-MPSP) based suboptimal guidance design with hard terminal and input inequality constraints is presented in this paper. Penalty function approach is followed with the G-MPSP algorithm to ensure input constraints. To demonstrate the robustness of the proposed guidance algorithm, the simulation results are carried out considering aerodynamic parameter uncertainties.

AB - The guidance design of aerobatic aircraft in air-race is to ensure several stringent terminal conditions at the race gates as well as to satisfy bounds on control and structural load factor. Also, it should be robust in presence of uncertainties in aerodynamic parameters. All these complexities make it a challenging problem. To meet these requirements, the generalized model predictive static programming (G-MPSP) based suboptimal guidance design with hard terminal and input inequality constraints is presented in this paper. Penalty function approach is followed with the G-MPSP algorithm to ensure input constraints. To demonstrate the robustness of the proposed guidance algorithm, the simulation results are carried out considering aerodynamic parameter uncertainties.

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M3 - Conference contribution

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BT - CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 3rd IEEE Conference on Control Technology and Applications, CCTA 2019

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Promod P, Maity A, Hong H, Bittner M, Holzapfel F. Aerobatic Aircraft Guidance Design for Air-Race Scenario. In CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications. Institute of Electrical and Electronics Engineers Inc. 2019. p. 795-800. 8920721. (CCTA 2019 - 3rd IEEE Conference on Control Technology and Applications). doi: 10.1109/CCTA.2019.8920721

Aerobatic Aircraft Guidance Design for Air-Race Scenario

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