PEER REVIEW 18th Australian International Aerospace Congress 27th International Symposium on Space Flight Dynamics Please select category below: Normal Paper Student Paper Young Engineer Paper Enhancement of the Spacecraft Attitude Dynamics Capabilities via Combination of the Inertial Morphing and Reaction Wheels (Keynote Paper and Presentation) Pavel M. Trivailo 1 and Hirohisa Kojima 3 1 RMIT University, School of Engineering, GPO Box 2476V, Melbourne, Victoria, 3001, Australia,
[email protected] 2 Tokyo Metropolitan University, Department of Aeronautics and Astronautics, Asahigaoka 6-6, Hino, Tokyo, Japan, 191-0065,
[email protected] Abstract In our previous works [1-4] we discovered an efficient method of control of the inversion of the spinning spacecraft. This method was prompted by the “Dzhanibekov’s Effect” or “Tennis Racket Theorem” [4], which are often seen by many as odd or even mysterious. The proposed spacecraft inversion method does not employ conventional RWs, but, instead, is using proposed morphing of the inertial properties of the spinning spacecraft. It allows to completely stop flipping motion or activate flipping motion on the spacecraft, being in its stable spin. In this paper, we are considering a spacecraft, which has both, inertial morphing and RW, capabilities. It is believed that performance of the RW systems could be enhanced with the inertial morphing. For general formulation, we first assume ability of the spacecraft to change its inertial properties, associated with all three principal axes of inertia. Secondly, we also assume that the spacecraft is equipped with three control wheels, located along the x, y and z- axes of the body-fixed frame.