Guidance-law synthesis for interception and rendezvous

Chi Ching Yang, Ciann-Dong Yang, Hsin Yuan Chen

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

In this paper, we consider guidance-law synthesis problems where the required conditions for interception or rendezvous are specified first, and a class of guidance laws is then synthesized to meet the given conditions. This approach is different from the existing analysis oriented methods where guidance laws are proposed first and then their performances are analyzed to check whether the interception or rendezvous conditions are satisfied. The synthesized guidance laws can be parametrized in terms of two free functions which provide additional design freedoms to satisify some strengthened interception or rendezvous conditions.

Original languageEnglish
Title of host publicationGuidance, Navigation, and Control Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
Pages154-159
Number of pages6
Publication statusPublished - 1998
EventGuidance, Navigation, and Control Conference and Exhibit, 1998 - Boston, United States
Duration: 1998 Aug 101998 Aug 12

Other

OtherGuidance, Navigation, and Control Conference and Exhibit, 1998
CountryUnited States
CityBoston
Period98-08-1098-08-12

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

Cite this

Yang, C. C., Yang, C-D., & Chen, H. Y. (1998). Guidance-law synthesis for interception and rendezvous. In Guidance, Navigation, and Control Conference and Exhibit (pp. 154-159). American Institute of Aeronautics and Astronautics Inc, AIAA.