Impact Angle Control for Planar Engagements
- Title
- Impact Angle Control for Planar Engagements
- Author
- 송택렬
- Keywords
- Aerospace; Transportation; Missiles; Control systems; Target tracking; Filters; State estimation; Aerodynamics; Performance analysis; Velocity control; Optimal control; Equations
- Issue Date
- 1999-12
- Publisher
- IEEE
- Citation
- IEEE Transactions on Aerospace and Electronic Systems IEEE Trans. Aerosp. Electron. Syst. Aerospace and Electronic Systems, IEEE Transactions on. 35(4):1439-1444 Oct, 1999
- Abstract
- A new and practical terminal guidance law is presented for impact angle control for two-dimensional active homing engagement scenarios. Impact angle control is required to enhance terminal effectiveness of antitank and antiship missile systems in particular. The proposed guidance law is developed to cope with missile velocity reduction due to aerodynamic drag and target maneuver. In actual applications, the proposed guidance law is combined in cascade with a target tracking filter under the certainty equivalence principle. The proposed guidance law in conjunction with the target tracking filter is shown to be effective in antiship active homing engagement scenarios by a series of Monte Carlo simulation runs.
- URI
- https://ieeexplore.ieee.org/document/805460/authors#authorshttps://repository.hanyang.ac.kr/handle/20.500.11754/171242
- ISSN
- 0018-9251
- DOI
- 10.1109/7.805460
- Appears in Collections:
- COLLEGE OF ENGINEERING SCIENCES[E](공학대학) > ELECTRICAL ENGINEERING(전자공학부) > Articles
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