Closed-Form Solution of Line-of-Sight Trajectory for Maneuvering Target

Closed-Form Solution of Line-of-Sight Trajectory for Maneuvering Target

In this study, an attempt is made to demonstrate that some scattered published results in the field of guidance theory can be derived directly from a general differential equation derived from classical mechanics. The approach offers the possibility of allowing a unified approach for various methods...

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Veröffentlicht in:Journal of guidance, control, and dynamics control, and dynamics, 2001-03, Vol.24 (2), p.408-409
1. Verfasser: Shoucri, Rachad M
Format: Artikel
Sprache:eng
Schlagworte:
Acceleration
Accuracy
Applied sciences
Computer science
control theory
systems
Continuum mechanics
Control system analysis
Control theory. Systems
Differential equations
Differentiation (calculus)
Electronic guidance systems
Exact sciences and technology
Maneuvering targets
Mechanics
Missiles
Satellites
Velocity
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Beschreibung
Zusammenfassung:In this study, an attempt is made to demonstrate that some scattered published results in the field of guidance theory can be derived directly from a general differential equation derived from classical mechanics. The approach offers the possibility of allowing a unified approach for various methods used to model the trajectory of a homing missile.
ISSN:0731-5090
1533-3884
DOI:10.2514/2.4726