The invention relates to a
surface plasmon DC pulse
attitude control and propulsion assisting
system for a hypersonic aircraft, and belongs to the technical field of aircraft power. Four pairs of
electrode strips arranged at upper, lower, left and right parts are vertically spaced apart and embedded in the outer surface of the aircraft in the
motion direction; each pair of
electrode strips consists of an IN1
electrode strip and an IN2 duality electrode strip; propulsion assisting and
attitude control can be realized by virtue of
surface plasmon DC pulses of the aircraft; two sets of DC pulse
plasmon drives are driven; the surface of the hypersonic aircraft is divided into four parts comprising the upper, lower, left and right parts; each of the parts is provided with two kinds of electrodes which are IN1 and IN2 electrodes; the two electrodes of each set are contrary to each other in
voltage, pulse and polarity; and a double-DC pulse
plasmon drive is driven. A DC pulse
plasmon driven PWM modulation
system takes an AT89S52 single-
chip microcomputer as a control core, and consists of a command input module, an
LED display module and a DC pulse power amplification drive module, thereby realizing digital precision control, completely changing the propulsion mode of the aircraft, saving more energy, eliminating the source of surface resistance of the aircraft in principle, and achieving great development potential.