• Title/Summary/Keyword: Optimal Re-entry Time

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One optimization on the flight trajectories of re-entry vehicle

  • Takano, Hiroyuki;Nakamura, Kazuki;Baba, Yoriaki
    • 제어로봇시스템학회:학술대회논문집
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    • 1996.10a
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    • pp.307-310
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    • 1996
  • In this paper, we deal with some numerical analyses of a re-entry vehicle in a 2-dimensional plane as an optimal control problem. To reduce the dynamic load, the heat load and the oscillation in the trajectory, we researched the trajectories in which the load factor or the rate of flight path angle was minimized during re-entry. In addition to that, taking advantage of the monotonous subarc method and the folded time-axis method, we tried to find the heat-less and load-less trajectory with combinations of some sectional functionals so that we can achieve more comfortability.

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When Do the Unemployed Jump in the Workforce?

  • Lee, Hyun-Tak;Jang, Bong-Gyu;Park, Seyoung
    • Management Science and Financial Engineering
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    • v.19 no.2
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    • pp.43-47
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    • 2013
  • This paper studies an optimal consumption and portfolio choice problem for unemployed people who have an option to work. Our problem is to find optimal consumption, risky investment, and workforce re-entry strategies for the unemployed. We find a closed form of the critical wealth level to re-enter the workforce. We show that the unemployed with a higher disutility of labor or a larger relative risk aversion are more reluctant to re-enter the workforce.

Simulation of Time-Delay Based Path-Tracking Control of Reusable Launch Vehicle (시간지연기법을 적용한 재사용발사체 유도제어 시뮬레이션)

  • Cho, Woosung;Lee, HyeongJin;Lee, Yeol;Ko, Sangho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.8
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    • pp.627-636
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    • 2021
  • This paper deals with a study for the guidance control of reusable launch vehicle. For this purpose, modeling of the equation of motion of a reusable launch vehicle with 6 degrees of freedom was performed. With this model, an optimal re-entry path was created and a path-following guidance control simulation was performed to follow the optimal re-entry path. For the design of the path-following guidance controller, the attitude controller applying a time-delay technique that is resistant to modeling uncertainty, disturbance and failure. And the nonlinear path-following guidance law were used. Guidance control simulation using a classical PD controller was performed and compared with the guidance control simulation of a reusable launch vehicle applying a time delay technique.