Research of integrated spiral maneuvering and guidance based on virtual target
To address the issue of interception, maneuvering, and precise guidance during the final stage of gliding flight, a study was conducted on the design of integrated maneuvering and guidance using a spiral trajectory as the focus. Firstly, the spiral trajectory was decomposed into an optimal reference...
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| Vydáno v: | Maǧallaẗ al-abḥath al-handasiyyaẗ Ročník 13; číslo 3; s. 2680 - 2688 |
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| Médium: | Journal Article |
| Jazyk: | angličtina |
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Elsevier B.V
01.09.2025
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| ISSN: | 2307-1877 |
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| Abstract | To address the issue of interception, maneuvering, and precise guidance during the final stage of gliding flight, a study was conducted on the design of integrated maneuvering and guidance using a spiral trajectory as the focus. Firstly, the spiral trajectory was decomposed into an optimal reference trajectory considering the glide angle constraint and a relative motion trajectory. Then, virtual circular moving targets were introduced to meet the requirements of spiral maneuvering and virtual trajectory moving targets were introduced to ensure trajectory convergence, based on the task division of different flight stages. Finally, the guidance rate of the reference trajectory was designed based on optimal control theory, and the guidance rate of the spiral maneuver was designed based on pure proportional guidance. Simulation results show that this guidance method can enable the vehicle to perform active spiral maneuvers, and control the landing deviation and impact angle deviation to within 2.5 m and 1 degree, respectively. |
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| AbstractList | To address the issue of interception, maneuvering, and precise guidance during the final stage of gliding flight, a study was conducted on the design of integrated maneuvering and guidance using a spiral trajectory as the focus. Firstly, the spiral trajectory was decomposed into an optimal reference trajectory considering the glide angle constraint and a relative motion trajectory. Then, virtual circular moving targets were introduced to meet the requirements of spiral maneuvering and virtual trajectory moving targets were introduced to ensure trajectory convergence, based on the task division of different flight stages. Finally, the guidance rate of the reference trajectory was designed based on optimal control theory, and the guidance rate of the spiral maneuver was designed based on pure proportional guidance. Simulation results show that this guidance method can enable the vehicle to perform active spiral maneuvers, and control the landing deviation and impact angle deviation to within 2.5 m and 1 degree, respectively. |
| Author | Lai, Canhui Lei, Gang Luo, Wei Wang, He |
| Author_xml | – sequence: 1 givenname: Wei surname: Luo fullname: Luo, Wei – sequence: 2 givenname: Gang surname: Lei fullname: Lei, Gang email: leig_123@163.com – sequence: 3 givenname: Canhui surname: Lai fullname: Lai, Canhui – sequence: 4 givenname: He surname: Wang fullname: Wang, He |
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| Cites_doi | 10.1016/j.ast.2019.03.002 10.1109/TAES.2016.150741 10.1016/j.ast.2018.03.038 10.1109/7.53445 10.2514/1.G003436 10.1016/j.ast.2015.03.016 10.1109/CCDC.2017.7978630 10.2514/1.G003518 10.1016/j.ast.2019.105427 10.1109/TAES.2010.5595614 10.2514/3.21658 10.2514/1.A33032 |
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| Issue | 3 |
| Keywords | Trajectory decomposition Virtual target Terminal guidance Spiral maneuvering |
| Language | English |
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