Non-ordinary state-based peridynamics (NOSBPD) has instability issue due to zero-energy modes during nodal integration. A zero-energy mode controlling scheme of NOSBPD for laminated composite materials is derived by using the linearized bond-based peridynamics, which forms a stable force state formulation corresponding to the non-uniform deformation. The proposed controlling scheme does not include any controlling parameter to avoid the complex parametric adjustment. A critical stretch continuously varying with the angle between fiber and bond directions is further proposed for the failure analysis of laminated composite materials with arbitrary fiber angles. The improved NOSBPD model adopts the explicit integration method to solve static problems. Several numerical examples are conducted to validate the proposed scheme suppressing the oscillation caused by zero-energy modes. K E Y W O R D S failure analysis, laminated composite materials, non-ordinary state-based peridynamics, stabilization, zero-energy modes 1 INTRODUCTION Peridynamics (PD) is a powerful non-local theory using integro-differential equations for differential equations. 1-5 The damage at any position in materials initiates spontaneously and can propagate along any paths. Based on these characteristics, PD has been widely used in damage and failure analysis of materials. 6-9 Generally, PD formulations have three types: bond-based peridynamics (BBPD), 10-13 ordinary state-based peridynamics (OSBPD), 14-16 and non-ordinary state-based peridynamics (NOSBPD). 17,18 BBPD has the restriction on the Poisson's ratio, and cannot distinguish the distortional and volumetric deformations. 4,19 OSBPD removes the restriction on the Poisson's ratio. Furthermore, NOSBPD uses the non-local approximate deformation gradient tensor to define strain. However, NOSBPD has inherent instability issues on displacement, stress, and strain fields due to zero-energy modes. 20,21 Recently, several zero-energy modes controlling methods have been developed for NOSBPD. 20-29 Littlewood 22 proposed a penalty approach to control zero-energy modes, in which the penalty force is proportional to the difference