TY - JOUR
T1 - Trajectory correcting method of fixed-canard dual-spin projectiles based on period average
AU - Xu, Nuo
AU - Yu, Jianqiao
AU - Wang, Yafei
N1 - Publisher Copyright:
©, 2015, AAAS Press of Chinese Society of Aeronautics and Astronautics. All right reserved.
PY - 2015/9/25
Y1 - 2015/9/25
N2 - A trajectory correcting scheme in which the value of the average control force can be regulated is made for a fixed-canard dual-spin projectile which is spin-stabilized. Hereby the guidance and control system of the projectiles is devised. Based on the high-speed rotation characteristic of fixed-canard dual-spin projectiles, the angular motion equation is simplified, and the angular motion is analyzed. Then the relation between the resultant normal force and the deflection angle of canards is obtained. Afterwards, a trajectory correcting method, whose trajectory correction component rote in diverse rotational speed or diverse amplitude to produce the average normal force whose value is controllable, is proposed based on the concept of period average. And the feasibility of the method is validated by 6-DOF ballistic simulation. The results indicate that, compared with the traditional method whose trajectory correction component is fixed, the new trajectory correcting method can continuously control the value and direction of the average normal force, thus the guidance and control of fixed-canard dual-spin projectiles is realized so as to eliminate the trajectory deviation and improve the precision.
AB - A trajectory correcting scheme in which the value of the average control force can be regulated is made for a fixed-canard dual-spin projectile which is spin-stabilized. Hereby the guidance and control system of the projectiles is devised. Based on the high-speed rotation characteristic of fixed-canard dual-spin projectiles, the angular motion equation is simplified, and the angular motion is analyzed. Then the relation between the resultant normal force and the deflection angle of canards is obtained. Afterwards, a trajectory correcting method, whose trajectory correction component rote in diverse rotational speed or diverse amplitude to produce the average normal force whose value is controllable, is proposed based on the concept of period average. And the feasibility of the method is validated by 6-DOF ballistic simulation. The results indicate that, compared with the traditional method whose trajectory correction component is fixed, the new trajectory correcting method can continuously control the value and direction of the average normal force, thus the guidance and control of fixed-canard dual-spin projectiles is realized so as to eliminate the trajectory deviation and improve the precision.
KW - Dual-spin
KW - Fixed-canard
KW - Guidance and control
KW - Period average
KW - Trajectory correcting method
UR - http://www.scopus.com/inward/record.url?scp=84946117121&partnerID=8YFLogxK
U2 - 10.7527/S1000-6893.2014.0354
DO - 10.7527/S1000-6893.2014.0354
M3 - Article
AN - SCOPUS:84946117121
SN - 1000-6893
VL - 36
SP - 2892
EP - 2899
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 9
ER -