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Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation
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| Zeitschriftentitel: | The Aeronautical Journal |
|---|---|
| Personen und Körperschaften: | , , |
| In: | The Aeronautical Journal, 123, 2019, 1267, S. 1437-1453 |
| Format: | E-Article |
| Sprache: | Englisch |
| veröffentlicht: |
Cambridge University Press (CUP)
|
| Schlagwörter: |
| author_facet |
Ai, X. L. Shen, Y. C. Wang, L. L. Ai, X. L. Shen, Y. C. Wang, L. L. |
|---|---|
| author |
Ai, X. L. Shen, Y. C. Wang, L. L. |
| spellingShingle |
Ai, X. L. Shen, Y. C. Wang, L. L. The Aeronautical Journal Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation Aerospace Engineering |
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ai, x. l. |
| spelling |
Ai, X. L. Shen, Y. C. Wang, L. L. 0001-9240 2059-6464 Cambridge University Press (CUP) Aerospace Engineering http://dx.doi.org/10.1017/aer.2019.71 <jats:title>ABSTRACT</jats:title><jats:p>This paper considers the integrated guidance and control (IGC) problem for impact angle constrained interception against manoeuvring targets with actuator saturation constraint. Based on the backstepping technique, an adaptive IGC law is presented to address this problem, where a fixed-time differentiator is proposed to estimate the derivatives of virtual control inputs to avoid the inherent problem of “explosion of complexity” suffered by the typical backstepping. Furthermore, an auxiliary first-order filter is introduced into the IGC law to cope with the actuator saturation constraint. The stability of the closed-loop system is strictly proved. Finally, the superiority of the proposed IGC law is verified by comparison simulations.</jats:p> Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation The Aeronautical Journal |
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| title |
Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_unstemmed |
Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_full |
Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_fullStr |
Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_full_unstemmed |
Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_short |
Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_sort |
adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| topic |
Aerospace Engineering |
| url |
http://dx.doi.org/10.1017/aer.2019.71 |
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2019 |
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1437-1453 |
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<jats:title>ABSTRACT</jats:title><jats:p>This paper considers the integrated guidance and control (IGC) problem for impact angle constrained interception against manoeuvring targets with actuator saturation constraint. Based on the backstepping technique, an adaptive IGC law is presented to address this problem, where a fixed-time differentiator is proposed to estimate the derivatives of virtual control inputs to avoid the inherent problem of “explosion of complexity” suffered by the typical backstepping. Furthermore, an auxiliary first-order filter is introduced into the IGC law to cope with the actuator saturation constraint. The stability of the closed-loop system is strictly proved. Finally, the superiority of the proposed IGC law is verified by comparison simulations.</jats:p> |
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| author | Ai, X. L., Shen, Y. C., Wang, L. L. |
| author_facet | Ai, X. L., Shen, Y. C., Wang, L. L., Ai, X. L., Shen, Y. C., Wang, L. L. |
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| description | <jats:title>ABSTRACT</jats:title><jats:p>This paper considers the integrated guidance and control (IGC) problem for impact angle constrained interception against manoeuvring targets with actuator saturation constraint. Based on the backstepping technique, an adaptive IGC law is presented to address this problem, where a fixed-time differentiator is proposed to estimate the derivatives of virtual control inputs to avoid the inherent problem of “explosion of complexity” suffered by the typical backstepping. Furthermore, an auxiliary first-order filter is introduced into the IGC law to cope with the actuator saturation constraint. The stability of the closed-loop system is strictly proved. Finally, the superiority of the proposed IGC law is verified by comparison simulations.</jats:p> |
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| series | The Aeronautical Journal |
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| spelling | Ai, X. L. Shen, Y. C. Wang, L. L. 0001-9240 2059-6464 Cambridge University Press (CUP) Aerospace Engineering http://dx.doi.org/10.1017/aer.2019.71 <jats:title>ABSTRACT</jats:title><jats:p>This paper considers the integrated guidance and control (IGC) problem for impact angle constrained interception against manoeuvring targets with actuator saturation constraint. Based on the backstepping technique, an adaptive IGC law is presented to address this problem, where a fixed-time differentiator is proposed to estimate the derivatives of virtual control inputs to avoid the inherent problem of “explosion of complexity” suffered by the typical backstepping. Furthermore, an auxiliary first-order filter is introduced into the IGC law to cope with the actuator saturation constraint. The stability of the closed-loop system is strictly proved. Finally, the superiority of the proposed IGC law is verified by comparison simulations.</jats:p> Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation The Aeronautical Journal |
| spellingShingle | Ai, X. L., Shen, Y. C., Wang, L. L., The Aeronautical Journal, Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation, Aerospace Engineering |
| title | Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_full | Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_fullStr | Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_full_unstemmed | Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_short | Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_sort | adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| title_unstemmed | Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation |
| topic | Aerospace Engineering |
| url | http://dx.doi.org/10.1017/aer.2019.71 |