Control Allocation Design of Reaction Control System for Reusable Launch Vehicle
During the early stage of reusable launch vehicle (RLV) reentry flight, reaction control system (RCS) is the major attitude control device. RCS, which is much different from the atmospheric steer’s control, requires a well designed control allocation system to fit the attitude control in high altitu...
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| Format: | Article |
| Language: | English |
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Wiley
2014-01-01
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| Series: | Abstract and Applied Analysis |
| Online Access: | http://dx.doi.org/10.1155/2014/541627 |
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| _version_ | 1832556641194606592 |
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| author | Rongjun Mu Xin Zhang |
| author_facet | Rongjun Mu Xin Zhang |
| author_sort | Rongjun Mu |
| collection | DOAJ |
| description | During the early stage of reusable launch vehicle (RLV) reentry flight, reaction control system (RCS) is the major attitude control device. RCS, which is much different from the atmospheric steer’s control, requires a well designed control allocation system to fit the attitude control in high altitude. In this paper, an indexed control method was proposed for RCS preallocation, a 0-1 integer programming algorithm was designed for RCS allocation controller, and then this RCS scheme’s effect was analyzed. Based on the specified flight mission simulation, the results show that the control system is satisfied. Moreover, several comparisons between the attitude control effect and RCS relevant parameters were studied. |
| format | Article |
| id | doaj-art-e18450ec4c1a464fbfe21799efb2d4e2 |
| institution | Kabale University |
| issn | 1085-3375 1687-0409 |
| language | English |
| publishDate | 2014-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | Abstract and Applied Analysis |
| spelling | doaj-art-e18450ec4c1a464fbfe21799efb2d4e22025-02-03T05:44:48ZengWileyAbstract and Applied Analysis1085-33751687-04092014-01-01201410.1155/2014/541627541627Control Allocation Design of Reaction Control System for Reusable Launch VehicleRongjun Mu0Xin Zhang1School of Astronautics, Harbin Institute of Technology, Harbin 150001, ChinaSchool of Astronautics, Harbin Institute of Technology, Harbin 150001, ChinaDuring the early stage of reusable launch vehicle (RLV) reentry flight, reaction control system (RCS) is the major attitude control device. RCS, which is much different from the atmospheric steer’s control, requires a well designed control allocation system to fit the attitude control in high altitude. In this paper, an indexed control method was proposed for RCS preallocation, a 0-1 integer programming algorithm was designed for RCS allocation controller, and then this RCS scheme’s effect was analyzed. Based on the specified flight mission simulation, the results show that the control system is satisfied. Moreover, several comparisons between the attitude control effect and RCS relevant parameters were studied.http://dx.doi.org/10.1155/2014/541627 |
| spellingShingle | Rongjun Mu Xin Zhang Control Allocation Design of Reaction Control System for Reusable Launch Vehicle Abstract and Applied Analysis |
| title | Control Allocation Design of Reaction Control System for Reusable Launch Vehicle |
| title_full | Control Allocation Design of Reaction Control System for Reusable Launch Vehicle |
| title_fullStr | Control Allocation Design of Reaction Control System for Reusable Launch Vehicle |
| title_full_unstemmed | Control Allocation Design of Reaction Control System for Reusable Launch Vehicle |
| title_short | Control Allocation Design of Reaction Control System for Reusable Launch Vehicle |
| title_sort | control allocation design of reaction control system for reusable launch vehicle |
| url | http://dx.doi.org/10.1155/2014/541627 |
| work_keys_str_mv | AT rongjunmu controlallocationdesignofreactioncontrolsystemforreusablelaunchvehicle AT xinzhang controlallocationdesignofreactioncontrolsystemforreusablelaunchvehicle |