This paper proposes distributed cooperative guidance laws for multiple missiles with
constant speeds to achieve impact-angle-constrained salvo attack against a stationary target …

A bias term to enhance proportional navigation is designed through an error signal that is a
function of pursuit angles with the objective of accommodating both the problem of impact …

This article presents the design of 3-D biased proportional navigation guidance laws for
arrival at a stationary target along a desired direction based on the spatial rotation of the …

PROPORTIONAL navigation (PN), the research on which can be traced back to decades
ago, is a guidance law that is known to feature both simplicity and reliability. There is a …

This dissertation focuses on the problem of impact time control by utilizing a new design
framework that is stated as shaping the fundamental states of the engagement via …

In this study, a three-dimensional formation flight guidance approach is developed. The
proposed method has three aspects to be considered: the formation geometry, the virtual …

This paper deals with controlling the impact time of a missile against its target by introducing
bias to the proportional navigation guidance law. The bias value, which is contained in an …

Bu çalışmada, çoklu otonom sistemler için güdüm algoritma tasarımları sunulmuştur.
Otonom sistem olarak jenerik bir füze ele alınmıştır. İlk olarak, eş zamanlı varış kontrolü için …

Pursuing prey through clutter is a complex and risky activity requiring integration of guidance
subsystems for obstacle avoidance and target pursuit. The unobstructed pursuit trajectories …

Artan operasyonel gereksinimlerden ötürü, yörünge şekillendirmesine ilişkin çalışmalarda
literatürde artış olmuştur. Füze güdümünün ilk ve temel amacı füzeyi hedefe sıfır kaçırma …