 Original Article
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 Published:
ClosedForm Modeling and Analysis of an XY FlexureBased NanoManipulator
Chinese Journal of Mechanical Engineering volume 31, Article number: 7 (2018)
Abstract
Flexurebased mechanisms are widely utilized in nano manipulations. The closedform statics and dynamics modeling is difficult due to the complex topologies, the inevitable compliance of levers, the Hertzian contact interface, etc. This paper presents the closedform modeling of an XY nanomanipulator consisting of statically indeterminate symmetric (SIS) structures using leaf and circular flexure hinges. Theoretical analysis reveals that the lever’s compliance, the contact stiffness, and the load mass have significant influence on the static and dynamic performances of the system. Experiments are conducted to verify the effectiveness of the established models. If no piezoelectric actuator (PEA) is installed, the influence of the contact stiffness can be eliminated. Experimental results show that the estimation error on the output stiffness and first natural frequency can reach 2% and 1.7%, respectively. If PEAs are installed, the contact stiffness shows up in the models. As no effective method is currently available to measure or estimate the contact stiffness, it is impossible to precisely estimate the performance of the overall system. In this case, the established closedform models can be utilized to calculate the bounds of the performance. The established closedform models are widely applicable in the design and optimization of planar flexurebased mechanisms.
1 Introduction
The integrations of piezoelectric actuators (PEAs) and flexurebased mechanisms have been widely utilized in nanopositioning and manipulations [1,2,3,4,5]. On the one hand, the shape of a PEA changes if charge or voltage is exerted, and thus generating subnanometer resolution actuation. However, PEAs suffer from the inherent hysteresis and creep nonlinearities [6,7,8]. Many feedforward and feedback methodologies have been proposed to compensate for the hysteresis and creep nonlinearities of PEAs [9, 10]. On the other hand, flexurebased mechanisms are capable of transmitting highprecision motions via the elastic deformations of the flexure hinges, making it ideal in building the transmission chains for PEAs [11, 12]. Widely utilized flexure hinge profiles include circular [13,14,15,16] and leaf [17, 18].
A single flexure hinge can be treated as a revolute joint during micro and nanoscale motions. In literature, many analytical and empirical models have been established for the compliance/stiffness of a single flexure hinge [19,20,21]. In order to improve the performance, multiple flexure hinges are generally combined in various configurations, such as the parallelograms [22,23,24] and the statically indeterminate symmetric (SIS) structures [25]. In these structures, it is common to treat the flexure hinges as flexible, and all the other components as rigid. Considering the widelyutilized lever mechanism as an example, the lever is frequently assumed to be rigid [26, 27] so as to facilitate the design and modeling processes. However, this assumption may increase the estimation error of the analytical model, especially when the lever is long or the compliance of the lever is not negligible.
A PEA is brittle and very weak when subjected to large lateral forces or torques. As a result, a PEA is not allowed to be firmly fixed to the mechanism during the installation. Many commercial PEAs use ball tips to eliminate the bending torques. In this case, a Hertzian contact interface forms between the tip and the mechanism. One significant drawback of Hertzian contact is its low contact stiffness that consumes large portion of the PEA’s displacement. The contact stiffness is highly dependent on the material properties and the contact status. Currently, there is no effective and reliable model to estimate the contact stiffness. Thus, the contact stiffness is frequently identified from the measured data [2].
As a flexurebased mechanism is generally light and compact, its performance is likely to be affected by the load mass, including the sensors, endeffectors, fixtures, and other accessories installed on the mechanism. The load mass increases the effective mass and moment of inertia of the system, leading to a slow response. Thus, the influence of the load mass should be taken into consideration in the design and modeling of flexurebased mechanisms.
This paper presents the closedform modeling of an XY flexurebased nanomanipulator developed in our previous work [28]. In this nanomanipulator, the flexure hinges are arranged in SIS configurations to transmit linear or angular motions. Analytical modeling reveals that the lever’s compliance significantly increases the estimation error. Thus, a threshold is proposed to determine whether the lever’s compliance can be neglected or not. Subsequently, a systematic modeling methodology is established to investigate the behavior of the nanomanipulator during linear and angular motions. Experimental results show that the modeling accuracy is significantly improved if the influence of the lever’s compliance, the contact stiffness, and the load mass is taken into consideration.
2 Design of the XY Nanomanipulator
An XY flexurebased nanomanipulator was developed for nano manipulation tasks in our previous work [28]. The schematic diagram and the geometric parameters of the nanomanipulator are presented in Figure 1, where a central platform is connected to four rigid linkages (consecutively labeled as linkage 1‒4) and then to the fixed frame through leaf springs. The nanomanipulator is symmetric in the x and yaxes, thus attenuating thermally induced errors and guaranteeing uniform characteristics. In each axis, the displacement of a PEA (P843.30 from Physik Instrumente) is magnified by a lever mechanism. Ball tip is selected to form a Hertzian contact interface so as to protect the PEA against the lateral forces and torques. Leaf and right circular flexure hinges are adopted in the manipulator. These flexure hinges are arranged into four different groups, namely Structure IIV (labeled as IIV in Figure 1). Except for Structure IV, the other structures are SIS structures with “clampedclamped” boundary conditions. Experimental results showed that the crossaxis coupling ratio of the nanomanipulator is below 1% [28].
3 Characteristics of the SIS Structures
3.1 Inplane Compliance of a Single Flexure Hinge
Leaf and right circular flexure hinges are utilized in the nanomanipulator. As illustrated in Figure 2, the geometric parameters are the hinge length 2L_{0} and the minimum thickness t. The shape functions of these hinges are defined in Eqs. (1) and (2), respectively:
where r is the radius of the circular profile, and for the rightcircular flexure hinge, r = L_{0}.
As shown in Figure 2, the inplane loads of the flexure hinge are the moment about the zaxis (M_{z}) and two forces in the x and yaxes (F_{x} and F_{y}). The angular deflection about the zaxis and the linear deflections in the x and yaxes are denoted as θ_{B}, u_{B}, and v_{B}, respectively. The bending moment M_{z}(x) and shear force Q(x) generated at position x may be written as
In the xaxis, the linear deflection at point B is defined by the following equation:
where E is the Young’s modulus, A(x) = 2dy(x) is the cross sectional area of the hinge, and
Subsequently, the angular deflection of point B about the zaxis can be modeled as
where I_{z}(x) = 2dy^{3}(x)/3 is the second moment of area with respect to zaxis, and
Timoshenko beam theory is utilized to calculate the linear deflection in yaxis:
where θ(x) denotes the angular deflection at position x, G is the shear modulus, κ is the Timoshenko shear coefficient, and
For hinges with a rectangular cross section, κ = 5/6.
Eqs. (4)‒(6) can be rewritten into a matrix form:
where matrix C is defined as the inplane compliance matrix of the flexure hinge.
In this paper, P_{1}‒P_{3} are only dependent on the geometric parameter of the hinge, and thus they are named as fundamental integrations.
3.2 Stiffness Modeling of the SIS Structures
Structure IIII can be schematically illustrated in Figure 3. It is obvious that static indeterminacy causes axial tension in lateral deformations, resulting in nonlinear loaddeflection relationship. However, the deflection of a flexurebased mechanism is very small when compared to the dimension of the mechanism. Thus, the above structural nonlinearity can be treated as negligible [25]. This is also adopted in this paper.
The reaction forces and moments of the SIS structure are defined in Figure 3. The static equilibrium conditions lead to the following equations:
There are six unknown variables in the above equations. For this statically indeterminate problem, the reactions of the structure can be solved using the flexibility method. If we remove the constraints from point B and treat the reactions F_{Bx}, F_{By}, and M_{Bz} as additional loads, the original statically indeterminate structure can be transformed into a statically determinate structure. The transformed structure is equivalent to the original structure only when the deflections of the transformed structure at point B are the same as the original structure. As a result, another three equations are derived:
where L_{01} = L_{0}+L_{1}.
Linear superposition is used to facilitate the calculation, and contribution of hinge 1 (or 2) refers to the deflections of point B when only hinge 1 (or 2) is treated as flexible. Utilizing Eqs. (8) and (9), we obtain the reaction forces and moments as below:
Similarly, we can obtain the deflections at point O using the linear superposition method, as shown below:
Subsequently, the inplane stiffness of the SIS structure can be derived from Eq. (11):
where k_{L}, k_{T} and k_{R} are the longitudinal, transverse, and angular stiffness, respectively.
Substituting P_{1}‒P_{3} into Eq. (12), the inplane stiffness of Structure IIII are obtained and provided in Table 1. It is found that the difference between the longitudinal and transverse stiffness is over 350 times. Therefore, these structures can be treated as rigid in the longitudinal direction. Table 1 also shows that Structure III is very stiff in the longitudinal and transverse directions. Thus, Structure III can be treated as an ideal revolute joint.
3.3 Stress Concentration of the SIS Structure
In Section 3.2, an SIS structure can be treated as rigid in the longitudinal direction. Thus, the normal stress caused by the axial load is not investigated herein. During the lateral deformations, the normal stress caused by the bending effect is the dominant stress. Thus, the maximum stress locates on the outer surface of the hinge. The maximum stress on the outer surfaces can be expressed using the following equation:
where k_{b} is the stress concentration factor for bending, σ_{max} and σ_{n} are the actual and nominal maximum stresses, respectively. For the leaf hinges in Structure I and II, the stress concentration has little influence on the bending compliance calculation according to DU’s work [29]. As a result, k_{ b } can be set to 1 for Structure I and II. For circular hinges in Structure III, according to the generalized model established in CHEN’s work [30], the stress concentration factor is calculated to be 1.030.
Due to the symmetry, hinge 1 is selected to calculate the maximum stress. Based on Figure 3, the inner moment at position x_{1} within hinge 1 is
Substituting Eqs. (10)‒(12) into Eq. (14), the relationship between M_{z}(x_{1}) and the SIS structure’s deflections is
In this manipulator, Structure I and II act as prismatic joints, i.e., θ_{O} = 0. In this case, substituting Eqs. (1) and (15) into Eq. (13), the following relationship is established:
On the other hand, Structure III functions as a revolute joint, and thus v_{O} = 0. Substituting Eqs. (2) and (15) into (13), the relationship between the σ_{ x } and v_{O} is established:
Eqs. (16) and (17) are utilized to obtain the maximum allowable deflections of the SIS structure. For Structure I and II, Eq. (16) shows that the maximum stress locates at both ends of the hinge. For Structure III, the location of the maximum stress can be obtained by differentiating Eq. (17) to x_{1}. Taking the yield strength of the material into consideration, the maximum allowable deflections of Structure IIII are calculated to be 1.46 mm, 1.30 mm, and 5.349 mrad, respectively.
4 Statics and Dynamics Modeling
Monolithic flexurebased mechanisms exhibit frictionless motions, resulting in an extremely low damping ratio. Hence, the nanomanipulator can be approximated as an undamped system. Based on Lagrange’s equation, the dynamics of a system can be expressed as follows:
where T and V denote the total kinetic and potential energy of the system, respectively; q_{ i } and Q_{ i } are the ith generalized coordinate and nonconservative force, respectively; and N is the number of generalized coordinates.
The first three modes of the nanomanipulator are the linear motions in the x and yaxes and the angular motion about the zaxis. The linear motions in each axis are the primary motions, whereas the angular motion about the zaxis is an unexpected motion degrading the motion accuracy. In this section, the dynamics models in both linear and angular motions are established.
4.1 Influence of the lever’s compliance
The lever in flexurebased mechanisms is typically treated as a rigid element [26, 27, 31] to facilitate the modeling process. This approximation may affect the estimated parameters of the overall system, e.g., the displacement amplification ratio. Figure 4(a) examines the lateral deformations of the lever in the nanomanipulator when a lateral force is applied at the free end. The contribution of Structure III is equivalent to a revolute joint with a torsional stiffness of k_{R3}. If the lever is assumed to be rigid, the free end moves to point C′. However, the lever is flexible, and the actual position of the free end is point C, with a distance of δ to point C′. The distance δ is negligible in very short levers while it becomes noticeable in long levers. In this paper, the equivalent structure shown in Figure 4(b) is proposed to account for the lever’s compliance, where k_{lever} is the equivalent lateral stiffness of the lever with “clampedfree” boundary conditions. The modeling of k_{lever} is straightforward using the mechanics of materials, and thus it is omitted for the conciseness of this paper. In the lever mechanism, k_{lever} is calculated to be 1.111 N/μm.
Figure 5(a) shows the deformation of the manipulator in the xaxis, where linkages 2 and 4 remain stationary, and the central platform, linkages 1 and 3 generate the same displacement. This corresponds to the first/second mode. The masses of the central platform, linkages 1 and 3 are denoted as m_{0}, m_{1}, and m_{3}, respectively. In the contact interface, point A is the end of the PEA and point B represents the contact point on the lever. The lumped mass model in the xaxis can be depicted in Figure 5(b), where m_{L} is the load mass, and I_{lever} denotes the moment of inertia of the lever. In Figure 5(b), the equivalent stiffness and the effective mass of the central platform are defined in the following equation:
From the static and dynamic point of view, the PEA is equivalent to an active force generator. In Figure 5(b), the equivalent stiffness, the driving force, and the effective mass of the PEA are denoted as k_{PEA}, F_{PEA}, and m_{PEA}, respectively; and k_{con} represents the equivalent contact stiffness of the contact interface. Further, a dimensionless parameter, η = k_{con}/k_{PEA}, is proposed to characterize the contact stiffness. Three generalized coordinates are defined in Figure 5(b), namely, the displacement of the PEA (x_{PEA}), the rotation angle of the lever (θ_{lever}), and the linear displacement of the central platform (x_{eq}).
In this nanomanipulator, the connection between the PEA and the lever is not firm, and preload force is utilized to keep the PEA and the lever in contact. The input stiffness k_{ in } is defined as the linear stiffness at point B when no PEA is installed. If k_{ in } is too low or the preload force is not large enough, the detachment phenomenon may occur in large step motions. However, if the input stiffness is too high, the displacement of the PEA will be significantly reduced. Based on Figure 5(b), k_{ in } can be calculated as follows:
The output stiffness is the linear stiffness of the central platform in the x or y axis that can be modeled as
The displacement amplification ratio of the lever mechanism is the ratio between the displacements of points C and B, which can be expressed as
The influence of the lever’s compliance is significant. If the lever is assumed to be rigid, k_{lever} converges to infinity. In this case, k_{in}, k_{out}, and k_{amp} will be overestimated. On the contrary, if the lever’s compliance is considered, the modeling complexity will increase significantly. Therefore, a criterion is necessary to to decide whether the lever’s compliance can be neglected or not. Based on Eqs. (20)‒(22), k_{lever} can only be neglected if the following two conditions are satisfied:
Eq. (23) is the criterion to decide whether the lever can be treated as rigid or not. In this nanomanipulator, k_{lever} = 11.7k_{eq} and h ^{2}_{3} k_{lever} = 0.618(h ^{2}_{2} k_{PEA}+k_{R3}). As a result, the lever’s compliance must be considered.
4.2 Dynamics of the Nanomanipulator in the xaxis
Based on Figure 5(b), the total kinematic and potential energy of the nanomanipulator are given below:
Substituting Eqs. (24) and (25) into Eq. (18), the nanomanipulator’s equations of motion in the xaxis are established as follows:
where
There are three modal vibrations for the linear motions in the xaxis. The corresponding natural frequencies can be numerically obtained using
As the nanomanipulator is not designed as a highspeed scanner, only the first natural frequency is investigated, and all the higher order dynamics is neglected. The influence of the contact stiffness and the load mass on the first natural frequency is analyzed and shown in Figure 6. The variation range of η is 10^{−3} to 10^{3}, corresponding to the cases of low and high contact stiffness, respectively. When the contact stiffness is low, the first natural frequency converges to its lower bound, corresponding to the case when no PEA is installed. When the contact stiffness increases, the first natural frequency gradually converges to its upper bound. When η > 100, the first natural frequency starts to converge. This indicates that the contact interface can be treated as rigid if η > 100. As the load mass increases the effective mass of the nano manipulator, its influence is also obvious in Figure 6: the first natural frequency decreases when the load mass increases.
4.3 Static Analysis of the Nanomanipulator
In static modeling, the velocities and accelerations are zero. Substituting these into Eq. (26), we can solve for the static relationships between the outputs and the input of the nanomanipulator, as shown below:
where x_{PEA0} = F_{PEA}/k_{PEA} is defined as the nominal displacement of the PEA (free extension without loads).
In order to investigate the influence of the contact stiffness on the nanomanipulator’s static characteristics, the following three dimensionless ratios are introduced to characterize the actual displacement of the PEA, the displacement applied to the lever, and the displacement of the central platform, respectively:
As Figure 7 illustrates, if the contact stiffness is low, g_{1} converges to its upper bound of 1, and both g_{2} and g_{3} converge to zero. As a result, the majority of the PEA’s displacement is not transmitted to the lever, but consumed in the contact interface. In contrast, if the contact stiffness is high, both g_{1} and g_{2} converge to k_{PEA}/(k_{in}+k_{PEA}), and g_{3} converges to its upper bound of k_{PEA}k_{amp}/(k_{in}+k_{PEA}). Therefore, in practice, it is desirable to improve the contact stiffness so as to achieve larger workspace.
4.4 Angular Motion of the Nanomanipulator
As illustrated in Figure 8(a), when a moment M_{z} is applied on the central platform, the central platform and all the linkages experience almost the same rotations, denoted as θ_{eq}. Figure 8(a) actually shows the third mode of the nanomanipulator. Based on the computational analysis, the lever mechanisms are almost stationary. Thus, this angular motion of the central platform has no effect on the PEAs, and the installations of the PEAs will not affect the angular behavior of the central platform.
The effective moment of inertia of the central platform, linkages 1 and 3 are denoted as I_{0}, I_{1}, and I_{3}, respectively. The corresponding rotation centers of linkages 1‒4 are labeled as O_{ i } (i = 1‒4). During the angular motion, the load mass will increase the central platform’s moment of inertia. If the load mass is assumed to be distributed uniformly across the central platform, the total kinematic energy of the nanomanipulator can be written as
where I_{ L }≈m_{ L }I_{0}/m_{0} is the moment of inertia of the load mass.
For Structure I, the deformation is a rotation about the zaxis. The deformation of Structure II is separated and illustrated with dashed lines in Figure 8(b1). The respective rotation centers are labeled as O′, O_{2}′, and O′_{4}. Since the leaf springs and linkages are connected in parallelogram configurations, during the angular motion, the distance between points O′ and O′_{4} is constant and equal to the distance between points O and O_{4}:
In Figure 8(b1), solid lines show a transformed structure obtained by counter rotating Structure II by an angle of −θ_{eq}. A further transformation is illustrated in Figure 8(b2): flipping the deformation of the lower flexure hinge. The above operations do not change the potential energy of Structure II. Thus, the angular deformation of Structure II is transformed to a linear deformation v_{O}. The relationship between v_{O} and θ_{eq} can be established based on the geometric constraints as below:
As illustrated in Figure 8(a), Structure IV rotates about point O_{3} during the angular motion. If an identical copy of Structure IV is connected to the opposite side, a new structure is obtained, as shown in Figure 8(c). The topology of the new structure is the same as SIS I. The deformation is an angular displacement of θ_{eq} about the zaxis.
Based on the above analyses, the total potential energy of the nanomanipulator is derived as follows:
where k ^{′}_{R4} is the angular stiffness of the new structure in Figure 8(c). In this manipulator, l_{5} = 12.32 mm. Utilizing Eq. (12), we have k ^{′}_{R4} = 7.272 N·m·rad^{−1}. Substituting Eqs. (31) and (34) into Eq. (18), the nanomanipulator’s equations of motion about the zaxis is established to be
Accordingly, the third natural frequency of the nanomanipulator can be calculated using
5 Experimental Verification
5.1 Experimental Setups
The static and dynamic characteristics of the nanomanipulator are experimentally investigated to verify the established models. Figure 9(a) shows the experimental setup for the static test, where the applied force and the resultant displacement of the central platform are measured. This corresponds to the output stiffness. The applied force is measured by a force gauge (HF10 from ALGOL), and the displacement is measured using a displacement probe (GT21 from TESA Technology). Figure 9(b) shows the experimental setup for the dynamic test, where a modal hammer (ENDEVCO 230110 from MEGGITT) is used to excite the nanomanipulator, and the response is measured by two accelerometers (4507B from Brüel & Kjær) installed on the central platform.
During the experimental tests, the parameters of the nanomanipulator with and without the PEAs installed are measured individually. In the installations of the PEAs, each PEA is boltfixed on the nanomanipulator, and the preload force is manually adjusted. Based on the previous analyses, higher contact stiffness is preferred during the installation. The load mass is not measured in the static test because it has no influence on the static parameters of the nanomanipulator. In the dynamic test, the load mass is measured to be 53.4 g, including the fixtures and two accelerometers.
5.2 Statics of the Nanomanipulator
The measured and estimated output stiffness of the nanomanipulator are listed in Table 2. If no PEA is not installed, the analytical results are obtained by substituting k_{PEA} = 0 and η = 0 into Eq. (21). In this case, the estimation error of the analytical model (Analytical 1) is only −2%. If the PEAs are installed, the output stiffness of the nanomanipulator increases. As η is an unknown variable, the lower and upper bounds of the analytical results are provided. The measured output stiffness in each axis is close to the upper bound of the analytical results, indicating that high contact stiffness is achieved.
In order to investigate the influence of the lever’s compliance, the analytical results with rigid lever assumption (Analytical 2) are also presented in Table 2 for the comparison. These analytical results are obtained by assigning k_{lever} a large value according to the criterion defined in Eq. (23). When no PEA is installed, the estimation error with rigid lever assumption is 42%. Such a high overestimation is not acceptable.
5.3 Dynamics of the Nanomanipulator
The frequency responses of the nanomanipulator are presented in Figure 10. Only the experimental results in the xaxis are presented due to the symmetry of the nanomanipulator. There are three peaks in the magnitude plot. The first peak corresponds to the first (or second) mode and the other two peaks are the unmodeled higher order dynamics. It is clearly illustrated that the installation of the PEAs only increases the first natural frequency.
The first natural frequencies in the x and yaxes are given in Table 3. Without the PEAs, the first natural frequency in the xaxis is measured to be 320 Hz. If the lever’s compliance is taken into consideration (Analytical 1), the estimation errors in the xaxis is 3.3%. When the PEAs are installed, the first natural frequency in the xaxis increase to 429 Hz. In this case, the lower and upper bounds of the analytical result are listed in Table 3. The measured first natural frequency is very close to the upper bound of the analytical result. This also demonstrates that high contact stiffness is achieved. Similarly, if the lever is assumed to be rigid (Analytical 2), the modeling accuracy is significantly affected. When no PEA is installed, the estimation error is 20.9%.
In current experimental setup, the third mode (rotations about the zaxis) doesn’t show up in the measured data. Therefore, the computational analysis is employed to evaluate the nanomanipulator’s behavior during the angular motions. Based on the computational results, the third natural frequency with the 53.4 g load mass is found to be 769.2 Hz. The analytical result is 754.1 Hz, corresponding to an estimation error of 2%, and thus validating the analytical model.
6 Conclusions

1.
An XY flexurebased nanomanipulator is presented in this paper. Two PEAs are employed to generate actuations and the crossaxis couplings are attenuated in the kinematic chains. The flexure hinges, arranged in SIS configurations, function as prismatic and revolute joints. Lever mechanism is utilized to magnify the displacement of the PEA. It is found that the lever’s compliance may significantly affect the estimated parameters of the nanomanipulator, such as the input/output stiffness and the first natural frequency. In this paper, a criterion is proposed to decide whether the lever’s compliance can be neglected or not. The lever’s compliance can be modeled by cascading a linear spring at the end of the lever. Although simple in formulation, this methodology is effective in improving the modeling accuracy, as verified through experimental results.

2.
The dynamics of the nanomanipulator in linear and angular motions is analyzed. The influence of the contact stiffness and the load mass is analytically investigated. Higher contact stiffness results in improved performances, such as larger workspace and higher first natural frequency. The influence of the load mass is also significant as it adds extra inertia to the nanomanipulator.

3.
The nanomanipulator is monolithically fabricated using wire electrical discharge machining technique. During the installation of the PEAs, the preload forces of the PEAs are manually tuned for a high contact stiffness. The analytical results show good modeling accuracy in comparison with the experimental results, and thus verifying the established models. The methodologies proposed in this paper are applicable in the design and optimization of flexurebased mechanisms.
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Authors’ contributions
YDQ designed the prototype, carried out the experiments and wrote the paper. XZ participated in the revision of the paper. BS participated in the design of experiments and revision of the paper. YLT and DWZ participated in the mechical design and manufacture of the prototype. All authors read and approved the final manuscript.
Authors' Information
YanDing Qin is currently an associate professor at Institute of Robotics and Automatic Information System, Nankai University, China. He received his PhD degree from Tianjin University, China, in 2012. His research interests include micro/nano manipulation and 3D bioprinting.
Xin Zhao is currently a professor at Institute of Robotics and Automatic Information System, Nankai University, China. He received PhD degree from Nankai University, China, in 1997. His research interests include micro operation robotics, MEMS, and biological pattern and tissue formation.
Bijan Shirinzadeh is currently a professor at Department of Mechanical and Aerospace Engineering, Monash University, Australia. He received his PhD degree from The University of Western Australia, Australia, in 1990. His research interests include micro/nano manipulation, systems kinematics and dynamics, haptics and roboticassisted surgery and microsurgery, and advanced manufacturing.
YanLing Tian is currently a professor at School of Mechanical Engineering, Tianjin University, China. He received his PhD degree from Tianjin University, China, in 2005. His research interests include micro/nano manipulation, mechanical dynamics, surface metrology and characterization
DaWei Zhang is currently a professor at School of Mechanical Engineering, Tianjin University, China. He received his PhD degree from Tianjin University, China, in 1995. His research interests include micro/nano positioning techniques, high speed machining methodologies, and dynamic design of machine tools.
Acknowledgements
Supported by National Natural Science Foundation of China (Grant Nos. 61403214, 61327802, U1613220), and Tianjin Provincial Natural Science Foundation of China (Grant Nos. 14JCZDJC31800, 14JCQNJC04700).
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Qin, YD., Zhao, X., Shirinzadeh, B. et al. ClosedForm Modeling and Analysis of an XY FlexureBased NanoManipulator. Chin. J. Mech. Eng. 31, 7 (2018). https://doi.org/10.1186/s100330180211z
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DOI: https://doi.org/10.1186/s100330180211z