The goal of this study was to utilize a quick and robust semi-empirical aerodynamics
prediction code (Missile DATCOM) to optimize and improve understanding of the flight …

Long range guided projectile systems require the advancement and integration of several
component technology areas to be successful. This work presents a detailed multi …

14. ABSTRACT A comprehensive aerodynamic dataset of a tail-controlled projectile was
generated to quickly evaluate and improve understanding of the flight performance of a long …

View Video Presentation: https://doi. org/10.2514/6.2021-0823. vid Improved
maneuverability for long-range projectiles is a key technology that enables both range …

View Video Presentation: https://doi. org/10.2514/6.2022-0612. vid In this paper, we present
an approach to flight control design for guided projectile applications with expanded flight …

In this investigation, we simulated and analyzed several configurations of generic high-
speed test vehicle with control effectors in the shape of rectangular prisms. The performance …

View Video Presentation: https://doi. org/10.2514/6.2021-0783. vid In this paper, an adaptive
control architecture using a recently developed direct uncertainty minimization approach is …

In this thesis, guided projectiles are studied in three aspects: a navigation system design,
CFD analysis of a guided projectile for low launch velocities and durability of electronic …

In the early stages of a new munition design process, it is desirable to quickly update the
controller as the aerodynamics and mass properties evolve. This allows for timely evaluation …

Recently, there has been increased interest on investigating technologies and
methodologies to extend the range of guided munitions for improved battlefield coverage …