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Volume 42 Issue 11
Nov.  2016
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Journal of Beijing University of Aeronautics and Astronautics  > 2016  >  42(11): 2540-2547.
YANG Ding, LIU Ming, YANG Lingxiao, et al. Energy suboptimal flight strategy of bank-to-turn maneuver for lifting vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(11): 2540-2547. doi: 10.13700/j.bh.1001-5965.2016.0613(in Chinese)
Citation: YANG Ding, LIU Ming, YANG Lingxiao, et al. Energy suboptimal flight strategy of bank-to-turn maneuver for lifting vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(11): 2540-2547. doi: 10.13700/j.bh.1001-5965.2016.0613(in Chinese)
shu

Energy suboptimal flight strategy of bank-to-turn maneuver for lifting vehicle

doi: 10.13700/j.bh.1001-5965.2016.0613
  • 1.

    College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

  • 2. Science and Technology on Space Physics Laboratory, Beijing 100076, China

  • Received Date: 20 Jul 2016
  • Rev Recd Date: 10 Aug 2016
  • Publish Date: 20 Nov 2016
    Abstract
  • When lifting vehicle is returning into earth's atmosphere, some path constraints including heating rate, dynamic pressure and overload should be enforced strictly. In order to reduce the energy losing during the performance of bank-to-turn maneuver, it is necessary to develop a suboptimal flight strategy. The main research contents of this paper are as follows. The trajectory characteristic of bank-to-turn maneuver is analyzed via studying the entry dynamics. The analytical solution to terminal velocity at the special terminal heading angle is derived. Furthermore, a suboptimal flight strategy, which considers the path constraints, is proposed based on this analytical solution. In order to verify the optimality of this flight strategy, a trajectory optimization problem is formulated so as to provide optimal energy trajectory. Then, Gauss pseudospectral method is used to solve this problem. The results show that both trajectories are highly consistent, and the flight strategy is more efficient and has greater engineering applicable values.

     

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