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Volume 41 Issue 12
Dec.  2015
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Journal of Beijing University of Aeronautics and Astronautics  > 2015  >  41(12): 2232-2239.
HAO Xianwei, WANG Yong, YANG Ye, et al. Optimization design of approach and landing trajectory for variable configuration RLV with multi-control surfaces[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(12): 2232-2239. doi: 10.13700/j.bh.1001-5965.2014.0822(in Chinese)
Citation: HAO Xianwei, WANG Yong, YANG Ye, et al. Optimization design of approach and landing trajectory for variable configuration RLV with multi-control surfaces[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(12): 2232-2239. doi: 10.13700/j.bh.1001-5965.2014.0822(in Chinese)
shu

Optimization design of approach and landing trajectory for variable configuration RLV with multi-control surfaces

doi: 10.13700/j.bh.1001-5965.2014.0822
  • 1.

    School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • 2. Beijing Aerospace Automatic Control Institute, Beijing 100854, China

  • Received Date: 29 Dec 2014
  • Rev Recd Date: 03 Apr 2015
  • Publish Date: 20 Dec 2015
    Abstract
  • To solve approach and landing problem of variable configuration reusable launch vehicle (RLV) with multi-control surfaces, a design method of approach and landing trajectory was proposed. The landing trajectory was divided into steep glide landing trajectory and flare landing trajectory. The controllable deflection limit of the aerodynamic surfaces and deep downturn quasi equilibrium equation constraints were considered and the steep glide landing trajectory optimization design was carried out. The RLV aerodynamic surface adjusting redundancy and variable configuration processes were considered, with constraint conditions of the gear down time, the flare normal overload and the grounding state, by the trajectory propagation based on the RLV dynamics equation, the optimal flare landing trajectory was designed and optimized. The steep glide landing trajectory and flare landing trajectory composed a complete approach and landing trajectory. Therefore, the designed approach and landing trajectory considered multi constraint conditions and improved the stability and safety of the landing process.

     

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