Results 41 to 50 of about 3,903 (185)
The SHarp Edge Flight EXperiment (SHEFEX) is a DLR program to investigate aerodynamic behaviour and thermal protection problems of re-entry vehicles at hypersonic velocities, using unconventional shapes comprising multi-facetted surfaces with sharp edges.
Turner, Peter +4 more
core
SINS/BDS tightly coupled integrated navigation algorithm for hypersonic vehicle. [PDF]
Chen K, Pei SS, Zeng CZ, Ding G.
europepmc +1 more source
Research on Hypersonic Vehicle Interception Conditions from a Small Velocity Ratio Perspective
To address the problem of hypersonic vehicle interception, taking the air-breathing hypersonic vehicle as the target of interception, this paper employs the concept of engagement geometry to theoretically provide the necessary conditions for the ...
Liu Shuangxi, Yan Binbin, Zhang Tong, Zhang Xu, Yan Jie
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Bionic adaptive fault-tolerant control of non-Gaussian stochastic attitude hypersonic vehicle. [PDF]
Hu KY, Zhu K, Sun W.
europepmc +1 more source
A generic rocket launcher geometry is studied experimentally and numerically at hypersonic flow conditions including a cold plume. The experiments are conducted in a hypersonic Ludwieg tube while numerical calculations are performed with a finite-volume
Oßwald, Kai +4 more
core
Adaptive Sliding Mode Fault Compensation for Sensor Faults of Variable Structure Hypersonic Vehicle. [PDF]
Hu KY, Yang C, Sun W.
europepmc +1 more source
Fuzzy adaptive fault diagnosis and compensation for variable structure hypersonic vehicle with multiple faults. [PDF]
Hu K, Li W, Cheng Z.
europepmc +1 more source
Modeling and simulation of a generic hypersonic vehicle [PDF]
Dissertation (Ph.D.)--University of Kansas, Aerospace Engineering, 2007.Horizontal take-off and horizontal landing hypersonic vehicles are a subject of great interest for future space launch missions.
Keshmiri, Shahriar
core
Hybrid Control Trajectory Optimization for Air-breathing Hypersonic Vehicle
Trajectory optimization problem for air-breathing hypersonic vehicle is addressed in this paper. The engine of hypersonic vehicle is assumed as a dual-mode scramjet engine which can be operated as a ramjet and scramjet for wide range of flight Mach ...
Song, Jaebong, Choi, Han-lim
core +1 more source
Hypersonic control effectiveness
The present study analyses the effects of a number of geometric parameters on the performance of a trailing edge control flap on a hypersonic body. The tests were conducted in a gun tunnel at Mach 8.2 and Mach 12.3.
Kumar, D, Kumar, D.
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