A sensor system and method of reducing plasma-induced communication inhibition for a main antenna includes using auxiliary antennas for detecting a density of plasma that affects operation of the main antenna, and re-orienting an electromagnetic field around the main antenna in response to the density detected to reduce effect of the plasma on the main antenna. The auxiliary antennas are also operable for data link communication and switchable such if the density of the plasma inhibits receipt or sending of signals by one of the auxiliary antennas, another one of the auxiliary antennas may be used for data link communication.
Method for plasma dynamic cancellation for hypersonic vehicles
2018-05-15
Patent
Electronic Resource
English
IPC: | H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS / B64C AEROPLANES , Flugzeuge / B64G Raumfahrt , COSMONAUTICS / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen / G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen / G01N Untersuchen oder Analysieren von Stoffen durch Bestimmen ihrer chemischen oder physikalischen Eigenschaften , INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES / H05H Plasmatechnik , PLASMA TECHNIQUE |
METHOD FOR PLASMA DYNAMIC CANCELLATION FOR HYPERSONIC VEHICLES
European Patent Office | 2019
|METHOD FOR PLASMA DYNAMIC CANCELLATION FOR HYPERSONIC VEHICLES
European Patent Office | 2017
|Potential hypersonic vehicles applications
AIAA | 1991
|Uncertainty analysis of flight dynamic characteristics for hypersonic vehicles
Online Contents | 2013
|