Guidance-law synthesis for interception and rendezvous

Chi Ching Yang; Ciann Dong Yang; Hsin Yuan Chen

doi:10.2514/6.1998-4115

Guidance-law synthesis for interception and rendezvous

Chi Ching Yang, Ciann Dong Yang, Hsin Yuan Chen

Department of Aeronautics and Astronautics

Research output: Contribution to conference › Paper › peer-review

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 language	English
Pages	154-159
Number of pages	6
DOIs	https://doi.org/10.2514/6.1998-4115
Publication status	Published - 1998
Event	Guidance, Navigation, and Control Conference and Exhibit, 1998 - Boston, United States Duration: 1998 Aug 10 → 1998 Aug 12

Other

Other	Guidance, Navigation, and Control Conference and Exhibit, 1998
Country/Territory	United States
City	Boston
Period	98-08-10 → 98-08-12

All Science Journal Classification (ASJC) codes

Electrical and Electronic Engineering
Aerospace Engineering
Control and Systems Engineering

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10.2514/6.1998-4115

Cite this

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title = "Guidance-law synthesis for interception and rendezvous",

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.",

author = "Yang, {Chi Ching} and Yang, {Ciann Dong} and Chen, {Hsin Yuan}",

note = "Publisher Copyright: Copyright {\textcopyright} 1998 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; Guidance, Navigation, and Control Conference and Exhibit, 1998 ; Conference date: 10-08-1998 Through 12-08-1998",

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doi = "10.2514/6.1998-4115",

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AU - Yang, Ciann Dong

AU - Chen, Hsin Yuan

PY - 1998

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AB - 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.

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T2 - Guidance, Navigation, and Control Conference and Exhibit, 1998

Y2 - 10 August 1998 through 12 August 1998

ER -

Guidance-law synthesis for interception and rendezvous

Abstract

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All Science Journal Classification (ASJC) codes

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