[HTML][HTML] Multidisciplinary design optimization of a dual-spin guided vehicle

J Karimi, MR Rajabi, SH Sadati, SM Hosseini - Defence Technology, 2024 - Elsevier
In this research, a Multidisciplinary Design Optimization approach is proposed for the dual-
spin guided flying projectile design considering external and internal parts of the body as …

Trajectory optimization of a subsonic unpowered gliding vehicle using control vector parameterization

A Mahmood, F Rehman, AI Bhatti - Drones, 2022 - mdpi.com
In many aero gliding vehicles, achieving the maximum gliding range is a challenging task. A
frequent example is the breakdown of an engine during flight or the use of unpowered stand …

Linear Parameter-Varying Polytopic Modeling and Control Design for Guided Projectiles

GM Vinco, O Sename, G Strub… - Journal of Guidance …, 2024 - arc.aiaa.org
In this paper, a linear parameter varying (LPV) modeling and control design approach is
applied to a new class of guided projectiles, aiming to exploit the advantages of the LPV …

A gain-scheduled approach for the control of a high-speed guided projectile

BC Gruenwald, J Bryson - AIAA Scitech 2022 Forum, 2022 - arc.aiaa.org
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 …

Linear Parameter Varying Pitch Autopilot Design for a class of Long Range Guided Projectiles

GM Vinco, S Theodoulis, O Sename… - AIAA SCITECH 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-2498. vid Promising results on LPV
design have been recently proposed, concerning the modeling and control of missiles …

Design methodology of a mini-missile considering flight performance and guidance precision

Z Licong, G Chunlin, S Hua… - Journal of Systems …, 2024 - ieeexplore.ieee.org
The design of mini-missiles (MMs) presents several novel challenges. The stringent mission
requirement to reach a target with a certain precision imposes a high guidance precision …

Comparison of aeroprediction methods for guided munitions

JL Paul, JD Vasile, J DeSpirito - AIAA Scitech 2021 Forum, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-0024. vid Several aeroprediction
methodologies were used to evaluate four munition configurations: a generic canard …

Concurrent Airframe-Controller Optimization of a Guided Projectile Fitted with Lifting Surfaces

V Riss, E Roussel, E Laroche - AIAA SCITECH 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0620. vid Innovative long-range
guided projectiles concepts require precise flight path tracking in order to achieve maximum …

Aeroballistic optimization of long-range guided ammunition

S Bagy, M Libsig, B Martinez, B Masse - International Journal of …, 2024 - emerald.com
Purpose This paper aims to describe the use of optimization approaches to increase the
range of near-future howitzer ammunition. Design/methodology/approach The performance …

Computational Investigation of Control Effectors on a Generic High-Speed Vehicle

JL Paul, J DeSpirito, J Sahu - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
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 …