Characterized as an MANNED UAV EDS HOVERCRAFT AIRPLANE OR SUBMARINE TRAVELING MACHINE CHASSIS FULL BODY structure electrical circuit architectural vertical stacked hollow open clearance metallic sheets and crystal sheets parallel frame structure ends are horizontally stacked hollow metallic sheets and crystal sheets position central enterceptive structure enterconnective hollow frame foundation bottom enclosures end and topped foundation enclosures functional likenesses as an electrical circuit EDT type ONE-WAY voltage SINGLE PHASE CURRENT CARRYING Rectifying electromagnet induction (PNPNPN) transistor (AC)(EDT)transductor(AC VOLTAGE transformer (AC/DC/ transducer OSCILLATING EDT horn PULSE EMI SONIC HFP DC/AC EMI EDT EDF EDS LINEAR SOLENOID MOTOR PULSE EMI SONIC PULSE ELECTRODYNAMICS SELF EMITTER PULSE PHASE REPEL SUSPENSION DRONE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEMS OR STRUCTURES POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE

Characterized as an MANNED UAV EDS HOVERCRAFT AIRPLANE OR SUBMARINE TRAVELING MACHINE CHASSIS FULL BODY structure electrical circuit architectural vertical stacked hollow open clearance metallic sheets and crystal sheets parallel frame structure ends are horizontally stacked hollow metallic sheets and crystal sheets position central enterceptive structure enterconnective hollow frame foundation bottom enclosures end and topped foundation enclosures functional likenesses as an electrical circuit EDT type ONE-WAY voltage SINGLE PHASE CURRENT CARRYING Rectifying electromagnet induction (PNPNPN) transistor (AC)(EDT)transductor(AC VOLTAGE transformer (AC/DC/ transducer OSCILLATING EDT horn PULSE EMI SONIC HFP DC/AC EMI EDT EDF EDS LINEAR SOLENOID MOTOR 
 PULSE EMI SONIC PULSE ELECTRODYNAMICS SELF EMITTER PULSE PHASE REPEL SUSPENSION DRONE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEMS OR STRUCTURES POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON 

MANNED UAV DC/AC PARALLEL VOLTAGE RECTIFING C-FRAME STACK VT METALLOID COMMUTATOR PNP SC VT EEG EFB AIRCRAFT CHASSIS MOTOR TRANSDUCTOR AIRPLANE ENCLOSURES HORN COMMON SC POWERED DC/AC POSITIVE IONIC GAUSS EMITTER MANNED MOBILITY VEHICLE ENGINE EDT EDF ESC EDS LINEAR SOLENOID ARIEL TRAVELING DRONE

Characterized as an MANNED UAV EDS HOVERCRAFT AIRPLANE OR SUBMARINE TRAVELING MACHINE CHASSIS FULL BODY structure electrical circuit architectural vertical stacked hollow open clearance metallic sheets and crystal sheets parallel frame structure ends are horizontally stacked hollow metallic sheets and crystal sheets position central enterceptive structure enterconnective hollow frame foundation bottom enclosures end and topped foundation enclosures functional likenesses as an electrical circuit EDT type ONE-WAY voltage SINGLE PHASE CURRENT CARRYING Rectifying electromagnet induction (PNPNPN) transistor (AC)(EDT)transductor(AC VOLTAGE transformer (AC/DC/ transducer OSCILLATING EDT horn PULSE EMI SONIC HFP DC/AC EMI EDT EDF EDS LINEAR SOLENOID MOTOR 

 PULSE EMI SONIC PULSE ELECTRODYNAMICS SELF EMITTER PULSE PHASE REPEL SUSPENSION DRONE SUBJECT NOT LIMITING TO ADDITIONAL SYSTEMS OR STRUCTURES POTENTIOMETRIC RANGE DESIGN INVENTOR JERMAINE MORTON

WEARABLE EXOSKELETRONIC EMI VT SC EDT EDF ESC EDS POWER BODY ARMOR MANNED UAV ORTHOSIS BIOMETRIC RANGE BRACE POWERED EDL BODY ARMOR DRONE 
BIOMECHATRONIC BRAINWAVES SWITCH CONTROLS AIRPLANE ENCLOSURES ACTING EDT TRANSDUCER TRANSDUCTOR MAGNETO HUMAN RADAR DOPPLER EFFECTS INTERFACES HUMAN BODY BRAINWAVES NEURON LOOP FEEDBACK SWITCH CONTROLS SEPARATE PIOLET HUMAN NERVE OR NEURON OSCILLATIONS. THE AIRPLANE ENCLOSURES EMI EEG SC ACEP EXTERIOR SURFACES ACTIVE VOLTAGE ONE-WAY RECTIFIER- ONE WAY VOLTAGE MOSFIT ENCLOSURES ELECTRONS EMITTER HEAT DOPING SEEBECK EFFECTS FARADAY'S CAGE ENCLOSURES EMT EMI VT SC EDT EDF ESC EDS LINEAR SOLENOID MANNED UAV ROTORLESS AIRPLANE DRONE DESIGN subject not limiting to additional systems or structure potentiometric range design inventor JERMAINE MORTON

This may be similar to the scale of an alien spacecraft pill structure shaped
Somewhat fundamental concepts alien Ariel dynamic technology aeronautic engineering aircraft system Hardware signals software based processing multiple relay channels switch output EMI FILTER 20,000HZ~ 500,000hz+ LOW NOISE hypersonic vibrations atmospheric electrophoresis acoustophoresis atmospheric electrolysis atmospheric faradays electrochemical thermal magneto hydro caloric thermal dynamics boyle's law Charles's Law atmospheric vapor dynamics between the medium rise rapid suspension from the source of radiation vapor suspension cloaking aircraft from visibile light spectrums blocking use's atmospheric vapor oscillator fogger generator infrared light blocking aircraft's armor exterior surfaces without light bouncing off of aircraft armor makes the visible spectrum of its light or shape impossible to see structure or design for parallel voltage thermal emissions subsystem circuit 400amphere+ induce electrons wavelength 1/4th of 1hz,1second voltage modulated electromotive FORCE PHASE INDUCTOR electromagnetic force pulse phase one way voltage Step Up sets of Transformer consist of positive charge DC pulse phase diamagnetic elements synchronous voltage induced DC AC phase ferromagnetic elements galvanized seebeck effect silicon quartz pyroelectric effect energy cell reactive magnetic flux electromagnetics hyper pulse electrodynamics Force phase paramagnetic element aircraft enclosures self- repel esc away ionic radiation vector field electromagnetic source of emission strengths wavelength forces against its weight of gravity or inertial mass as to levitation as to fly

UFO 
https://youtu.be/n36KOqbwrMY?si=O2IMlVPxy52kVVDl