Analysis of Nonlinear Missile Guidance Systems Through Linear Adjoint Method
نویسندگان
چکیده
منابع مشابه
Guidance Law Evaluation for Missile Guidance Systems
In missile guidance system, to reduce the interception “miss distance,” it is important to choose a suitable guidance law and navigation constant. This paper investigates and compares the system behavior of guidance laws under different navigation constants. Based on use of the adjoint technique, miss distance sensitivity analyses which consider the system noise, target step maneuver, initial h...
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ژورنال
عنوان ژورنال: Smart Science
سال: 2015
ISSN: 2308-0477
DOI: 10.1080/23080477.2015.11670488