Analysis of 9-D Filter and Observability Enhanced Guidance Law as Applied to Hit-To-Kill Missiles

Michael W. Dancer; S. N. Balakrishnan

Analysis of 9-D Filter and Observability Enhanced Guidance Law as Applied to Hit-To-Kill Missiles

Michael W. Dancer
, S. N. Balakrishnan

Missouri University of Science and Technology

Research output: Contribution to journal › Article › peer-review

Abstract

In this day and age, the need for an ever more reliable missile defense system is becoming increasingly apparent. This need for increased reliability leads to the need for improving existing guidance, control, and estimation architectures. This paper analyzes a new suboptimal filter, 6-D, coupled with a guidance law specifically designed on enhance system observability during hit-to-kill applications. The results presented herein demonstrate the potential effectiveness of the filter/guidance combination against highly maneuvering, evasive targets.

Original language	American English
Journal	Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit (2006, Keystone, CO)
State	Published - Aug 24 2006

Keywords

Architecture
Missile Defense

Disciplines

Aerospace Engineering
Mechanical Engineering

Cite this

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title = "Analysis of 9-D Filter and Observability Enhanced Guidance Law as Applied to Hit-To-Kill Missiles",

abstract = " In this day and age, the need for an ever more reliable missile defense system is becoming increasingly apparent. This need for increased reliability leads to the need for improving existing guidance, control, and estimation architectures. This paper analyzes a new suboptimal filter, 6-D, coupled with a guidance law specifically designed on enhance system observability during hit-to-kill applications. The results presented herein demonstrate the potential effectiveness of the filter/guidance combination against highly maneuvering, evasive targets.",

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year = "2006",

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journal = "Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit (2006, Keystone, CO)",

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AU - Dancer, Michael W.

AU - Balakrishnan, S. N.

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Y1 - 2006/8/24

N2 - In this day and age, the need for an ever more reliable missile defense system is becoming increasingly apparent. This need for increased reliability leads to the need for improving existing guidance, control, and estimation architectures. This paper analyzes a new suboptimal filter, 6-D, coupled with a guidance law specifically designed on enhance system observability during hit-to-kill applications. The results presented herein demonstrate the potential effectiveness of the filter/guidance combination against highly maneuvering, evasive targets.

AB - In this day and age, the need for an ever more reliable missile defense system is becoming increasingly apparent. This need for increased reliability leads to the need for improving existing guidance, control, and estimation architectures. This paper analyzes a new suboptimal filter, 6-D, coupled with a guidance law specifically designed on enhance system observability during hit-to-kill applications. The results presented herein demonstrate the potential effectiveness of the filter/guidance combination against highly maneuvering, evasive targets.

KW - Architecture

KW - Missile Defense

UR - https://scholarsmine.mst.edu/mec_aereng_facwork/2109

M3 - Article

JO - Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit (2006, Keystone, CO)

JF - Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit (2006, Keystone, CO)

ER -

Analysis of 9-D Filter and Observability Enhanced Guidance Law as Applied to Hit-To-Kill Missiles

Abstract

Keywords

Disciplines

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