This article proposes inverse dynamic calculation methods for actuator control of deployable structures and adaptive structures in space. The objective of this study is to estimate time change of an input moment controlled by an actuator which can gradually stop the transformation without acceleration and velocity at an assumed position and time so as not to cause structural vibration after the transformation. This article proposes three types of specific inverse calculation methods using trigonometric function and higher degree equations with their calculation examples which may be useful for design of an actuator considering deceleration control.
CraigJJ.Introduction to robotics: mechanics and control. 2nd ed.Boston, MA: Addison-Wesley Publishing Company, 1989.
10.
WieB.Space vehicle dynamics and control. 2nd ed.Reston, VA: American Institute of Aeronautics and Astronautics, 2008.
11.
TsaiLW.Solving the inverse dynamics of a Stewart-Gough manipulator by the principle of virtual work. J Mech Des: T ASME2000; 122(1): 3–9.
12.
StaicuSLiuXJWangJ.Inverse dynamics of the HALF parallel manipulator with revolute actuators. Nonlinear Dynam2007; 50(1–2): 1–12.
13.
EnferadiJTootoonchiAA.Inverse dynamics analysis of a general spherical star-triangle parallel manipulator using principle of virtual work. Nonlinear Dynam2010; 61(3): 419–434.
14.
StaicuS.Matrix modeling of inverse dynamics of spatial and planar parallel robots. Multibody Syst Dyn2012; 27(2): 239–265.
15.
GlaserPE.Power from the sun: its future. Science1968; 162(3856): 857–861.
16.
DOE/NASA. Program assessment report statement of findings: satellite power systems concept development and evaluation program. Report no. DOE/ER-0085, 1November1980. Washington, DC: NASA.
TakatsukaM.Dynamic inverse analysis of scissors structure for its deployment control in space. In: Proceedings of the IASS-SLTE 2014 symposium, the international association for shell and spatial structures, Brasilia, Brazil, 15–19 September 2014.
