“长空”超低空无人驾驶飞机的飞行控制系统

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1990, Vol. 11 ›› Issue (6): 261-268.

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FLIGHT CONTROL SYSTEM OF THE "CHANG-KONG" SUPER-LOW ALTITUDE PILOTLESS AIRCRAFT

Luo Feng, Xia Yuncheng

Nanjing Aeronautical Institute

Received:1988-11-07 Revised:1900-01-01 Online:1990-06-25 Published:1990-06-25

Abstract

Abstract: The paper introduces the flight control system of the pilotless aircraft. This is the first time in our country that an autopilot equipped in a domestic target plane employs single-chip microcomputers. The arrangement of the control system, the control laws of the system and the measures we took to improve the altitude accuracy in the super-low flight mode are described. The demonstration flight test shows that the design of this hybrid autopilot is fully successful.

Key words: target plane, pilotless aircraft, flight control, super`low altitude

Luo Feng;Xia Yuncheng. FLIGHT CONTROL SYSTEM OF THE "CHANG-KONG" SUPER-LOW ALTITUDE PILOTLESS AIRCRAFT[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(6): 261-268.

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FLIGHT CONTROL SYSTEM OF THE "CHANG-KONG" SUPER-LOW ALTITUDE PILOTLESS AIRCRAFT

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