Parameterized Design and Dynamic Analysis of a Reusable Launch Vehicle Landing System with Semi-Active Control

نویسندگان
چکیده

برای دانلود باید عضویت طلایی داشته باشید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Analysis and Design of Launch Vehicle Flight Control Systems

This paper describes the fundamental principles of launch vehicle flight control analysis and design. In particular, the classical concept of “drift-minimum” and “load-minimum” control principles is re-examined and its performance and stability robustness with respect to modeling uncertainties and a gimbal angle constraint is discussed. It is shown that an additional feedback of angle-of-attack...

متن کامل

Reusable Launch Vehicle Design Implications for Regeneration Time Thesis

In the last few years, the Air Force Research Laboratory (AFRL) sponsored several research projects on a Reusable Launch Vehicle (RLV) whose design, operation, and logistics requirements are intended to be much simpler than for the Space Shuttle. As part of these efforts, the previous researchers developed a discrete-event simulation model, called Maintenance, Integration, and Launch Pad Operat...

متن کامل

Evaluation of a Landing Gear Semi-active Control System for Complete Aircraft Landing

This paper deals with the simulation of landing gear semi-active control for a small trainer aircraft in a multibody framework. The behavior of single passive landing gear drop test simulation models and of a complete aircraft landing simulation model, developed and implemented in the commercial multibody code ADAMS in previous works, is compared to the that of analogous models equipped with se...

متن کامل

Automatic Landing Guidance Systems and Design of an Optimal Landing Control System

Guidance and control of aircraft in the landing phase imposes extra pilot work loads, hence application of automatic landing control systems is of great importance. In this study automatic landing control systems are introduced and an optimal landing control system is designed. The control system performance criteria are based on minimum control effort. The designed system is simulated for a tr...

متن کامل

A Study of Arts: a Dual-fuel Reusable Launch Vehicle with Launch Assist

An independent assessment of the Advanced Reusable Transportation System (ARTS) has been conducted. The ARTS concept is an all-rocket, fully reusable launch vehicle utilizing electromagnetic launch assist. ARTS is fitted with a dual-fuel main propulsion system utilizing flight proven Space Shuttle Main Engines and RD-180s. Nominally, the vehicle is intended to operate without a crew using auton...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Symmetry

سال: 2020

ISSN: 2073-8994

DOI: 10.3390/sym12091572