Optimal three-dimensional impact time guidance with seeker’s field-of-view constraint
| Autor: | Shaoming He, Antonios Tsourdos, Hyo-Sang Shin, Chang-Hun Lee |
|---|---|
| Rok vydání: | 2021 |
| Předmět: |
0209 industrial biotechnology
Missile guidance Computer science Mechanical Engineering Optimal error dynamics Impact time Control (management) Aerospace Engineering TL1-4050 Field of view Impact time control 02 engineering and technology 01 natural sciences 010305 fluids & plasmas Constraint (information theory) Field-of-view constraint Nonlinear system 020901 industrial engineering & automation Control theory 0103 physical sciences Proportional navigation Limit (mathematics) Applied optimal control Motor vehicles. Aeronautics. Astronautics |
| Zdroj: | Chinese Journal of Aeronautics, Vol 34, Iss 2, Pp 240-251 (2021) |
| ISSN: | 1000-9361 |
| DOI: | 10.1016/j.cja.2020.04.006 |
| Popis: | This paper proposes a new three-dimensional optimal guidance law for impact time control with seeker’s Field-of-View (FOV) constraint to intercept a stationary target. The proposed guidance law is devised in conjunction with the concept of biased Proportional Navigation Guidance (PNG). The guidance law developed leverages a nonlinear function to ensure the boundedness of velocity lead angle to cater to the seeker’s FOV limit. It is proven that the impact time error is nullified in a finite-time under the proposed method. Additionally, the optimality of the biased command is theoretically analyzed. Numerical simulations confirm the superiority of the proposed method and validate the analytic findings. |
| Databáze: | OpenAIRE |
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