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
Flight Mechanics and Control
2005-05-09
77 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
SLUB | 1962
|Springer Verlag | 2018
|Springer Verlag | 2016
|SLUB | 2007
|TIBKAT | 1996
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