| Lie-group integration method for constrained multibody systems in state space Z Terze, A Müller, D Zlatar Multibody system dynamics 34, 275-305, 2015 | 90 | 2015 |
| The significance of the configuration space Lie group for the constraint satisfaction in numerical time integration of multibody systems A Müller, Z Terze Mechanism and Machine Theory 82, 173-202, 2014 | 48 | 2014 |
| Forward dynamics of open-loop multibody mechanisms using an efficient recursive algorithm based on canonical momenta J Naudet, D Lefeber, F Daerden, Z Terze Multibody System Dynamics 10, 45-59, 2003 | 46 | 2003 |
| Null space integration method for constrained multibody systems with no constraint violation Z Terze, D Lefeber, O Muftić Multibody System Dynamics 6, 229-243, 2001 | 46 | 2001 |
| Geometric properties of projective constraint violation stabilization method for generally constrained multibody systems on manifolds Z Terze, J Naudet Multibody System Dynamics 20, 85-106, 2008 | 38 | 2008 |
| Singularity-free time integration of rotational quaternions using non-redundant ordinary differential equations Z Terze, A Müller, D Zlatar Multibody system dynamics 38 (3), 201-225, 2016 | 35 | 2016 |
| On the choice of configuration space for numerical Lie group integration of constrained rigid body systems A Müller, Z Terze Journal of computational and applied mathematics 262, 3-13, 2014 | 28 | 2014 |
| Geometric methods and formulations in computational multibody system dynamics A Müller, Z Terze Acta mechanica 227, 3327-3350, 2016 | 26 | 2016 |
| Structure of optimized generalized coordinates partitioned vectors for holonomic and non-holonomic systems Z Terze, J Naudet Multibody system dynamics 24, 203-218, 2010 | 24 | 2010 |
| Discrete mechanics and optimal control optimization of flapping wing dynamics for Mars exploration Z Terze, V Pandža, M Kasalo, D Zlatar Aerospace science and technology 106, 106131, 2020 | 20 | 2020 |
| An angular momentum and energy conserving Lie-group integration scheme for rigid body rotational dynamics originating from Störmer–Verlet algorithm Z Terze, A Mueller, D Zlatar Journal of computational and nonlinear dynamics 10 (5), 051005, 2015 | 18 | 2015 |
| An angular momentum and energy conserving Lie-group integration scheme for rigid body rotational dynamics originating from Störmer–Verlet algorithm Z Terze, A Mueller, D Zlatar Journal of computational and nonlinear dynamics 10 (5), 051005, 2015 | 18 | 2015 |
| Multibody dynamics: computational methods and applications Z Terze Springer, 2014 | 18 | 2014 |
| General formulation of an efficient recursive algorithm based on canonical momenta for forward dynamics of closed-loop multibody systems J Naudet, D Lefeber International Design Engineering Technical Conferences and Computers and …, 2005 | 15 | 2005 |
| Optimized Flapping Wing Dynamics via DMOC approach Z Terze, V Pandža, M Kasalo, Z Dario Nonlinear Dynamics, 2020 | 13 | 2020 |
| Aircraft attitude reconstruction via novel quaternion-integration procedure Z Terze, D Zlatar, V Pandža Aerospace science and technology 97, 105617, 2020 | 12 | 2020 |
| Numerical simulation of landing aircraft dynamics Z Terze, M Vrdoljak, H Wolf Strojarstvo: časopis za teoriju i praksu u strojarstvu 51 (6), 657-665, 2009 | 8 | 2009 |
| Differential-geometric modelling and dynamic simulation of multibody systems A Müller, Z Terze Strojarstvo: Journal for Theory and Application in Mechanical Engineering 51 …, 2009 | 7 | 2009 |
| Dynamical stability of the response of oscillators with discontinuous or steep first derivative of restoring characteristic H Wolf, Z Terze, A Sušić European Journal of Mechanics-A/Solids 23 (6), 1041-1050, 2004 | 7 | 2004 |
| Lie Group Forward Dynamics of Fixed-Wing Aircraft With Singularity-Free Attitude Reconstruction on SO(3) Z Terze, D Zlatar, M Vrdoljak, V Pandža Journal of computational and nonlinear dynamics 12 (2), 021009, 2017 | 6 | 2017 |
