Motion control problems for multimode unmanned aerial vehicles

被引:3
作者
Syrov, A. S. [1 ]
Puchkov, A. M. [1 ]
Rutkovskii, V. Yu. [2 ]
Glumov, V. M. [2 ]
机构
[1] Mars Moscow Expt Design Bur, Moscow, Russia
[2] Russian Acad Sci, Trapeznikov Inst Control Sci, Moscow, Russia
关键词
Aircraft control - Unmanned aerial vehicles (UAV) - Flight control systems - Adaptive control systems - Altitude control - Antennas;
D O I
10.1134/S0005117917060121
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper considers flight control specifics for modern unmanned aerial vehicles with paths described by a wide range of altitudes, including super-aerodynamic flights. It is noted that this type of aerial vehicles belongs to multimode dynamic objects with varying characteristics in the course of their operation. Adaptive control methods used in control systems for unmanned aerial vehicles are overviewed. Finally, adaptive control capabilities are studied for the vehicle's angular position in gliding and cruising modes under combined jet reaction and aerodynamic control.
引用
收藏
页码:1128 / 1137
页数:10
相关论文
共 21 条
  • [1] Abadeev E.M., 2012, OSNOVY FORMIROVANIYA
  • [2] Byushgens G.S., 1998, Aerodinamika, ustoichivost' i upravlyaemost' sverkhzvukovykh samoletov (Aerodynamics, Stability, and Controllability of Supersonic Aircraft)
  • [3] Emelyanov S.Y., 2009, IZBRANNYE T, V1
  • [4] Eskin A.F., 2009, OSNOVY PROEKTIROVANI
  • [5] Glumov V.M., 2000, IZV ROSS AKAD NAUK T, P120
  • [6] Kolesnikov A.A, 2013, NOVYE NELINEINYE MET
  • [7] KRASOVSKII AA, 1987, SPRAVOCHNIK TEORII A
  • [8] Lebedev A. A., 1973, DINAMIKA POLETA BESP
  • [9] Puchkov A.M., 2012, P INT C SYST ID CONT, P896
  • [10] Puchkov A.M., 1996, AVIAKOSM TEKHN TEKHN, P36