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Optimal Guidance Anticipating Missile Performance

Grimm, W. and Well, K.H. (1991) Optimal Guidance Anticipating Missile Performance. In: Proc. AGARD Guidance and Control Panel. AGARD Panel 53rd. Symposium "Air Vehicle Mission Control and Management", Amsterdam, 22.-25.10.91.

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Two different guidance methods are designed for the pre-launch phase in a one-versus-one air combat situation with missiles. In both guidance schemes a missile/target simulation is performed to estimate the miss distance at the end of a fictitious missile launch. A way to do this in real time is described. The first guidance method continuously evaluates the miss distance for each aircraft against the respective opponent. The guidance is such that the ratio of the rates of the miss distances takes an optimal value from the view of the guided aircraft. Thus, it reaches a firing opportunity first. The purpose of the second guidance method is to reach a firing position against a nonmaneuvering target in minimum time.

Item URL in elib:https://elib.dlr.de/27847/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1991, pages=13,
Title:Optimal Guidance Anticipating Missile Performance
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Journal or Publication Title:Proc. AGARD Guidance and Control Panel
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Guidance methods; Missile/target simulation; Firing opportunity.
Event Title:AGARD Panel 53rd. Symposium "Air Vehicle Mission Control and Management", Amsterdam, 22.-25.10.91
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
DLR - Research theme (Project):UNSPECIFIED
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Robotics and Mechatronics (until 2012) > Institut für Dynamik der Flugsysteme
Deposited By: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 06:47

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