Corrigendum to “Attitude control of towed space debris using only tether” [Acta Astronaut. 138 (2017) 152-167]

Low‐Velocity Impact Response Analysis of Functionally Graded Piezoelectric Plates Using Finite‐Element Method and a Two‐Degrees‐of‐Freedom Spring‐Mass Model

“…It was highlighted that the size of stability regions and amplitude of steady‐state oscillations are significantly correlated with the volume fraction and distribution pattern of the carbon nanotube, temperature field, as well as initial geometrical imperfection. Wang [ 62 ] considered the effect of material porosity on the vibrational response of the FGP plates in various translational speeds and highlighted the importance of porosity factor, porosity distribution pattern, and the volume fraction of constituents on the nonlinear vibrational response of the porous FGP plates. Su et al [ 63 ] investigated the vibrational characteristics of the rectangular FGP plates with general boundary conditions by applying the penalty function method and FSDT.…”

Nonlinear buckling of axially compressed FG‐GRCL stiffened cylindrical panels with a piezoelectric layer by using Reddy's higher‐order shear deformation theory

“…Thus, the influences of piezoelectric layers on the nonlinear buckling and postbuckling of the FG-GRCL plates by using TSDT or HSDT and considering the von Karman strains are recently studied. Numerous articles [33][34][35][36][37][38] investigated the vibration, [33][34][35] the stability, [36] the bending, [37] and static and dynamic behavior [38] of the FGM with piezoelectric layers subjected to electromechanical or thermal load.…”