| contributor author | An Wang | |
| contributor author | Qinghua Zeng | |
| contributor author | Likun Ma | |
| contributor author | Hongfu Wang | |
| date accessioned | 2022-02-01T00:26:22Z | |
| date available | 2022-02-01T00:26:22Z | |
| date issued | 9/1/2021 | |
| identifier other | %28ASCE%29AS.1943-5525.0001263.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4271437 | |
| description abstract | The response difference between the classical mathematical model of a ducted rocket and a real experiment is compared in this study, and a new revised method is proposed based on the free volume. A virtual free volume that is related to the real free volume is built to eliminate the discrepancy between the model and experiment, and a possible explanation of virtual free volume is carried out. In addition, design constraints and variation characteristics of the ducted rocket control system are analyzed. Furthermore, a radial basis function (RBF) adaptive control method is proposed to deal with the variation. Finally, hardware in a loop simulation device for the ducted rocket control system is presented, and its reliability is proved by analysis and comparison with a direct-connected ground test, and a serial simulation test that consistent with the numerical simulation is carried out to verify the validation of the controller. | |
| publisher | ASCE | |
| title | Virtual Free-Volume Revised Method and Adaptive Control for Solid Ducted Rockets | |
| type | Journal Paper | |
| journal volume | 34 | |
| journal issue | 5 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0001263 | |
| journal fristpage | 04021053-1 | |
| journal lastpage | 04021053-16 | |
| page | 16 | |
| tree | Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 005 | |
| contenttype | Fulltext | |
