The present invention provides a stealth high maneuvering target aircraft and a method for controlling a stealth high maneuvering target aircraft, which relates to the technical field of unmanned aerial vehicles and solves the technical problem existing in the prior art that the stealth characteristic of the target aircraft is poor and the stealth design and the comprehensive matching degree between the stealth design and the flight performance of the target aircraft is not high. The stealth high maneuvering target aircraft comprises a fuselage, a wing, a vertical tail, a horizontal tail and a "clam-type" air inlet provided under the ventral of the fuselage. The wing is provided in the middle of the fuselage and belongs to the lower single-wing layout. The vertical and horizontal tails are provided at the tail of the fuselage; a method for controlling the stealth high maneuvering target aircraft confirms a dynamic model with high accuracy and high confidence; uses the combined control of overload and attitude to ensure stable flight control of large overload; and uses overload, speed, angle of attack, and sideslip angle by the control system. The present invention can overcome the problem of poor stealth characteristics of the existing target aircraft, and can solve the problem that the comprehensive matching degree between the stealth design and the flight performance of the target aircraft is not high.
STEALTH LARGE MANEUVERING TARGET AIRCRAFT AND CONTROL METHOD FOR STEALTH LARGE MANEUVERING TARGET AIRCRAFT
GROSSES MANÖVRIERENDES TARNKAPPENZIELFLUGZEUG UND STEUERUNGSVERFAHREN FÜR GROSSES MANÖVRIERENDES TARNKAPPENZIELFLUGZEUG
AÉRONEF FURTIF DE GRANDE MANOEUVRE CIBLE ET PROCÉDÉ; DE COMMANDE POUR AÉRONEF FURTIF DE GRANDE MANOEUVRE CIBLE
2021-11-10
Patent
Elektronische Ressource
Englisch
Airborne radar for high maneuvering stealth target
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