Adaptive control system for separation of aircraft motion on roll and sideslip

    Research output: Chapter in Book/Report/Conference proceedingChapter

    Abstract

    The requirements to maneuver a modern aircraft involve the development and realization of advanced control of a longitudinal and lateral aircraft motion. The manual control system for independent motion control of an aircraft on rolling and sideslip angles is given in [1]. The system depends upon a real-time measurement of air-dynamic coefficients of the aircraft, or requires the information from the tabulated parameters on all regimes of the aircraft motion. However, methods of precise measurement of air-dynamic coefficients in non-stationary conditions of the aircraft motion are not yet available at the present time. The exact parameters for all regimes of the aircraft motion cannot be obtained from a-priory measurements either. Therefore, a complete decoupled motion of an aircraft cannot be achieved. In this paper the solution for a decoupled motion of an aircraft is obtained in the class of non-searching adaptive control systems with a reference model [2]. The new algorithms developed in this paper achieve a decoupled motion with desirable dynamic precision even in the conditions of high non-stationary of parameters. The robustness of the control system to the interaction of subsystems is accomplished as well.
    Original languageEnglish
    Title of host publication2nd International Symposium on Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008
    PublisherIEEE
    Pages1-4
    ISBN (Print)978-1-4244-3908-9
    DOIs
    Publication statusPublished - 2008
    Event2nd International Symposium on Systems and Control in Aerospace and Astronautics - Shenzhen, China
    Duration: 10 Dec 200812 Dec 2008

    Conference

    Conference2nd International Symposium on Systems and Control in Aerospace and Astronautics
    Abbreviated titleISSCAA 2008
    CountryChina
    CityShenzhen
    Period10/12/0812/12/08

    Fingerprint

    Adaptive control systems
    Aircraft
    Control systems
    Manual control
    Motion control
    Air
    Time measurement
    Robustness (control systems)

    Bibliographical note

    This paper is not available on the repository. It was given at 2nd International Symposium on Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008, 10-12 Dec 2008, Shenzhen

    Keywords

    • air-dynamic coefficients
    • decoupled motion
    • independent motion control
    • lateral aircraft motion
    • longitudinal aircraft motion
    • nonsearching adaptive control systems
    • real-time measurement

    Cite this

    Vershinin, Y. (2008). Adaptive control system for separation of aircraft motion on roll and sideslip. In 2nd International Symposium on Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008 (pp. 1-4). IEEE. https://doi.org/10.1109/ISSCAA.2008.4776325

    Adaptive control system for separation of aircraft motion on roll and sideslip. / Vershinin, Yuri.

    2nd International Symposium on Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. IEEE, 2008. p. 1-4.

    Research output: Chapter in Book/Report/Conference proceedingChapter

    Vershinin, Y 2008, Adaptive control system for separation of aircraft motion on roll and sideslip. in 2nd International Symposium on Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. IEEE, pp. 1-4, 2nd International Symposium on Systems and Control in Aerospace and Astronautics, Shenzhen, China, 10/12/08. https://doi.org/10.1109/ISSCAA.2008.4776325
    Vershinin Y. Adaptive control system for separation of aircraft motion on roll and sideslip. In 2nd International Symposium on Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. IEEE. 2008. p. 1-4 https://doi.org/10.1109/ISSCAA.2008.4776325
    Vershinin, Yuri. / Adaptive control system for separation of aircraft motion on roll and sideslip. 2nd International Symposium on Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. IEEE, 2008. pp. 1-4
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    abstract = "The requirements to maneuver a modern aircraft involve the development and realization of advanced control of a longitudinal and lateral aircraft motion. The manual control system for independent motion control of an aircraft on rolling and sideslip angles is given in [1]. The system depends upon a real-time measurement of air-dynamic coefficients of the aircraft, or requires the information from the tabulated parameters on all regimes of the aircraft motion. However, methods of precise measurement of air-dynamic coefficients in non-stationary conditions of the aircraft motion are not yet available at the present time. The exact parameters for all regimes of the aircraft motion cannot be obtained from a-priory measurements either. Therefore, a complete decoupled motion of an aircraft cannot be achieved. In this paper the solution for a decoupled motion of an aircraft is obtained in the class of non-searching adaptive control systems with a reference model [2]. The new algorithms developed in this paper achieve a decoupled motion with desirable dynamic precision even in the conditions of high non-stationary of parameters. The robustness of the control system to the interaction of subsystems is accomplished as well.",
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    AB - The requirements to maneuver a modern aircraft involve the development and realization of advanced control of a longitudinal and lateral aircraft motion. The manual control system for independent motion control of an aircraft on rolling and sideslip angles is given in [1]. The system depends upon a real-time measurement of air-dynamic coefficients of the aircraft, or requires the information from the tabulated parameters on all regimes of the aircraft motion. However, methods of precise measurement of air-dynamic coefficients in non-stationary conditions of the aircraft motion are not yet available at the present time. The exact parameters for all regimes of the aircraft motion cannot be obtained from a-priory measurements either. Therefore, a complete decoupled motion of an aircraft cannot be achieved. In this paper the solution for a decoupled motion of an aircraft is obtained in the class of non-searching adaptive control systems with a reference model [2]. The new algorithms developed in this paper achieve a decoupled motion with desirable dynamic precision even in the conditions of high non-stationary of parameters. The robustness of the control system to the interaction of subsystems is accomplished as well.

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