Finite Time Horizon Analysis of Launch Vehicles Under Mass and Thrust Uncertainty

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

Finite time stabilization of time-delay nonlinear systems with uncertainty and time-varying delay

In this paper, the problem of finite-time stability and finite-time stabilization for a specific class of dynamical systems with nonlinear functions in the presence time-varying delay and norm-bounded uncertainty terms is investigated. Nonlinear functions are considered to satisfy the Lipchitz conditions. At first, sufficient conditions to guarantee the finite-time stability for time-delay nonl...

متن کامل

Thrust Vector Control Robustness of axial-symmetric Launch Vehicles with Fuel Slosh

Clearance of Thrust Vector Control (TVC) laws for launchers demands the capability to provide analytical certificates for the system’s robust stability. During exo-atmospheric flight, a key role is played by the ability to deal with non rigid-body effects such as fuel sloshing. Depending on its frequency and magnitude, sloshing can easily deteriorate the performance of the TVC laws to the point...

متن کامل

Economic Uncertainty of Weight and Market Parameters for Advanced Space Launch Vehicles

Market sensitivity and weight-based cost estimating relationships are key drivers in determining the financial viability of advanced space launch vehicle designs. Due to decreasing space transportation budgets and increasing foreign competition, it has become essential for financial assessments of prospective launch vehicles to be performed during the conceptual design phase. As part of this fi...

متن کامل

Stress Analysis of Flight Vehicles under Flight Conditions

A method is presented for the stress analysis of flight vehicles under different flight conditions including gust and control surface deflection (or maneuver) using the governing equations of rigid-body motions and elastic deformations. The Lagrangian approach is used to derive the governing equations of motions. For this purpose, the basic equations of motions are derived in terms of potential...

متن کامل

Robustness in the face of polytopic initial conditions uncertainty and polytopic system matrices uncertainty in finite-horizon linear H∞-analysis

This paper addresses a linear finite-horizon robust optimal H∞ analysis problem, where the system matrices and the system initial conditions (ICs, x0) are concurrently uncertain, both in a polytopic manner. Current finite-horizon H∞ analysis practice assumes x0 ∈R ; that is, allows infinite ICs uncertainty. This assumption is unrealistically conservative, and incompatible with the prevalent rob...

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: IFAC-PapersOnLine

سال: 2020

ISSN: 2405-8963

DOI: 10.1016/j.ifacol.2020.12.1296