Aerotecnica Missili & Spazio
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Các bài báo tiêu biểu
Evaluation of Regression Rate Enhancing Concepts and Techniques for Hybrid Rocket EnginesAbstract The low regression rate of Hybrid Rocket Engines (HREs) is one prominent characteristic that is addressed in most abstracts concerning hybrid propulsion. Over the years, researchers developed and investigated numerous ways to tackle the low regression rate problem of HREs. This article is a collection and assessment of these diverse methods and designs. It ... ...
- 2022
Gain Selection for Attitude Stabilization of Earth-Pointing Spacecraft Using MagnetorquersAbstract This paper considers a feedback control law that achieves attitude stabilization for Earth-pointing spacecraft using only magnetorquers as torque actuators. The control law is proportional derivative (PD)-like with matrix gains, and it guarantees asymptotic stability. The PD matrix gains are determined through the numerical solution of a periodic linear qua... ...
Tập 100 Số 1 - Trang 15-24 - 2021
Wind Tunnel Aerodynamic Study of a VTOL-UAV for Wide Range of Angles of Attack and Sideslip Angles
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Pilot in the Loop Simulation of Helicopter-Ship Operations Using Virtual Reality
Tập 99 Số 1 - Trang 53-62 - 2020
Application of the Sequential Gradient Restoration Algorithm to the Solution of the Low Thrust Transfer Problem
Tập 96 Số 4 - Trang 228-236 - 2017
Non-linear modelling for Multi-Disciplinary and Multi-Objective Optimization of a complete aircraft
Tập 92 Số 1-2 - Trang 61-68 - 2013