공력 및 측추력을 이용한 유도탄의 혼합제어기 설계
- Title
- 공력 및 측추력을 이용한 유도탄의 혼합제어기 설계
- Other Titles
- Mixed Control of Agile Missile with Aerodynamic Fin and Thrust Vectoring Control
- Author
- 송택렬
- Keywords
- Linear Time-Varying Control(선형 시변 제어); Dynamic Inversion(역동역학기법); Control Allocation(제어분배법칙); Autopilot(자동조정장치); Missile(유도탄)
- Issue Date
- 2003-11
- Publisher
- 군사과학기술학회
- Citation
- 한국군사과학기술학회지, v. 6, no. 3, page. 122-130
- Abstract
- This paper is concerned with a control allocation strategy using the dynamic inversion and the pseudo inverse control which generates the nominal control input trajectories, and autopilot design using time-varying control technique which is time-varying version of pole placement of linear time-invariant system for an agile missile with aerodynamic fin and thrust vectoring control. Control allocation of this paper is capable of extracting the maximum performance from each control effector, aerodynamic fin and thrust vectoring control, by combining the action of them. Time-varying control technique for autopilot design enhance the robustness of the tracking performance for a reference command. The main results are validated through the nonlinear simulation.
- URI
- https://www.dbpia.co.kr/Journal/articleDetail?nodeId=NODE09689599https://repository.hanyang.ac.kr/handle/20.500.11754/156428
- Appears in Collections:
- COLLEGE OF ENGINEERING SCIENCES[E](공학대학) > ELECTRICAL ENGINEERING(전자공학부) > Articles
- Files in This Item:
There are no files associated with this item.
- Export
- RIS (EndNote)
- XLS (Excel)
- XML