| Abstract: | Design of the attitude control system is facing obstacles as it aims not only at the stability control at the starting flight phase when initial attitude error and aerodynamic interference are inevitable, but also at the continuous attitude control with wide angle at the release phase.Due to the limit of the spatial arrangement of attitude control''s dynamical system and the limit of the control of the arm of force, attitude control system design is not an easy work considering the time pressure and the shortage of the project fund.Despite all these difficulties, attitude control design team, relying on canard reaction force controlling design technique and multi-tunnel continuous wide angle attitude adjusting design technique, etc., has successfully come up with an optimal solution package, thus making significant contribution to the research work and the flight experiment. |
