首页> 外文会议>2016 2nd International Conference on Control Science and Systems Engineering >Model predictive control guidance for constrained mars pinpoint landing
【24h】

Model predictive control guidance for constrained mars pinpoint landing

机译:约束火星精确着陆的模型预测控制指导

获取原文
获取原文并翻译 | 示例

摘要

In order to achieve pinpoint landing under various constraints during powered descent phase of landing on Mars, model predictive control (MPC) is employed in this paper by designing a novel performance index. Its main advantage is that it can ensure the pinpoint landing with online calculation and handle constraints as well, both of which are important in practical engineering missions. Detailed derivational process is given. Simulation results show the effectiveness of the proposed guidance.
机译:为了在火星着陆动力下降阶段在各种约束条件下实现精确着陆,本文通过设计一种新颖的性能指标,采用了模型预测控制(MPC)。它的主要优点是可以通过在线计算确保精确着陆并处理约束,这两者在实际工程任务中都很重要。给出了详细的推导过程。仿真结果表明了所提出指导的有效性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号