This chapter contains sections titled:

    Safety Improvement for Two‐Stage‐to‐Orbit Vehicles by Appropriate Mission Abort Strategies

    Introduction

    Dynamics Model of Two‐Stage‐to‐Orbit Vehicle

    Optimization Problem

    Safety Improved Nominal Trajectory

    Mission Aborts of Carrier Stage

    Mission Aborts of Orbital Stage

    Mission Abort Plan

    Conclusions

    Optimal Trajectories for Hypersonic Vehicles with Predefined Levels of Inherent Safety

    Introduction

    Theoretical Background

    Classical Problem

    Related Boundary Value Problem

    Extended Problem (A)

    Extended Problem (B)

    Numerical Method

    Model System

    Overview

    Thrust Model

    Atmospheric and Aerodynamic Model

    Equations of Motion

    Primary Problem

    Secondary Problem

    Extended Problem (B)

    Numerical Results

    Conclusion

    Hypersonic Trajectory Optimization for Thermal Load Reduction

    Introduction

    Modelling of Vehicle Dynamics

    Modelling of Heat Input

    Optimization Problem

    Results

    Range Cruise

    Return‐to‐Base Cruise

    Conclusions

    Flight Dynamics and Control Problems of Two‐Stage‐to‐Orbit Vehicles

    Flight Tests and Simulation Experiments for Hypersonic Long‐Term Dynamics Flying Qualities

    Introduction

    Hypersonic Flight Dynamics

    Research Aircraft and Flight Simulator

    Results

    Conclusions

    Wind Tunnel Tests for Modelling the Separation Dynamics of a Two‐Stage‐to‐Orbit Vehicle

    Introduction

    Test Facility and Wind Tunnel Models

    Results

    Conclusions


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    Titel :

    Flight Mechanics and Control


    Beteiligte:


    Erscheinungsdatum :

    2005-05-09


    Format / Umfang :

    77 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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