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Online midcourse guidance method for boost phase interception via adaptive convex programming

  • Published:2021-11 Issue: Volume:118 Page:107037
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Yang BiaoORCID,Jing Wuxing,Gao Changsheng

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

1. Generic analysis of interceptor design and tracking system performance for boost phase intercept;Ohlmeyer,2010

2. Trajectory-shaping guidance for interception of ballistic missiles during the boost phase;Lukacs;J. Guid. Control Dyn.,2008

3. Kill vehicle guidance and control sizing for boost-phase intercept;Zarchan;J. Guid. Control Dyn.,2012

4. Two-stage cooperative guidance strategy using a prescribed-time optimal consensus method;Zhang;Aerosp. Sci. Technol.,2020

5. Guidance laws for boost-phase interception of ballistic missile;Ge;J. Northwest. Polytech. Univ.,2013

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