Robust vibration control of a flexible manipulator in presence of payload uncertainty
Muhammad Atif Khushnood^{1} , Xiaogang Wang^{2} , Naigang Cui^{3}
^{1, 2, 3}Harbin Institute of Technology, Harbin, China
^{1}Corresponding author
Journal of Vibroengineering, Vol. 19, Issue 5, 2017, p. 35423555.
https://doi.org/10.21595/jve.2017.18215
Received 30 January 2017; received in revised form 15 March 2017; accepted 24 April 2017; published 15 August 2017
This paper presents the results of hybrid vibration controllers applied for vibration suppression of flexible manipulator. The model of the manipulator is assumed to be uncertain due to varying payload. To cater for the model uncertainty the proposed hybrid controller combines robust input shaping for command input with $\mu $controller applied for active vibration suppression using smart materials. Dependence of hybrid controller performance on design frequencies of input shaper is also studied. Results showed that the performance of hybrid controller is strongly dependent on the parameters used for designing input shaper, and the effectiveness of the hybrid controller can be substantially increased by judiciously selecting the design frequencies of input shaper. Effectiveness of the proposed controller is demonstrated by comparative studies with hybrid controllers formed by robust input shaping and PPF (positive position feedback) controller. Results are compared for suppressing vibrations resulting from slewing motion of manipulator, where the slewing motion is controlled by the PD controller. Results of comparisons showed that the μcontroller gave better performance in terms of settling time and energy consumption than those using PPF.
Keywords: flexible manipulator, input shaping, active vibration control, positive position feedback (PPF), μsynthesis.
1. Introduction
Space structures ranging from spacecraft itself to robots employed for their servicing and other associated tasks are essentially light weight structures. The light weight of these structures combined with their large size results in low frequency modes which could be excited during the necessary maneuvering of these structures. Since, these structures have to fulfill very stringent performance requirements the vibratory motion of these structures resulting from excitation of low frequency fundamental modes needs to be suppressed as early as possible.
To overcome this problem the early research in this area was focused on input shaping. Initially developed by O. J. M. Smith [1], input shaping is an openloop technique for vibration suppression that relies on modifying input command by convolving it with a sequence of impulses whose vibrations are selfcanceling (see section input shaping). The main advantage of input shaping is its simple design and implementation. Unlike other methods for vibration control which require complex system models, design of input shaper only requires damping and natural frequencies of the modes to be suppressed. Moreover, due to its openloop nature its implementation doesn’t require any measurement sensor. These advantages have led to vast research in this area which ranges from: (a) improving robustness of input shaper to uncertainty in system natural frequencies; (b) incorporation of auxiliary constraints, such as minimum maneuver time, fuel usage, and transient deflection limits; and (c) implementation on various systems, such as spacebased antennas, cranes, flexible manipulators and spacecraft. A comprehensive review on this subject is provided in [2]. However, a major limitation of command shaping, due to absence of feedback loop is that in presence of modeling uncertainties complete elimination of vibrations is not possible.
With the advent of piezoelectric actuators vibration attenuation by using feedback control became particularly attractive for space applications. Fast response, high stiffness, low weight, large operating bandwidth and low power consumption are some of the characteristics which make these actuators suitable for space applications [3]. A number of control techniques have been employed by the researchers for vibration reduction by using feedback control. A comprehensive review of the employed techniques can be found in [4, 5]. However, due to its high vibration attenuation and stability characteristics, PPF is by far the most widely used control technique.
Residual vibrations can be completely eliminated by feedback control, whereas, input shaping can provide considerable reduction in vibration without using extra actuator, sensor and energy. Hence, development of hybrid controllers was a natural outcome. A hybrid controller based on command shaping and PPF was used by [6], results showed the effectiveness of the proposed controller in comparison with either of command shaping and feedback control alone. However, as input shaping and PPF can only guarantee performance for a limited variation in system parameters, the method was not suitable for systems with unknown or largely varying frequencies. To overcome this problem adaptive input shaping is proposed by [79]. Instead of adaptive input shaping a hybrid controller with adaptive PPF control and robust input shaping is proposed by [10]. One drawback associated with adaptive techniques either applied for input shaping or feedback control is the realtime computational burden. Moreover, the time required for parameter estimation may result in overall large settling time, because for the multimode case and persistent excitation simultaneous parameter estimation and control may possibly lead to erroneous results [11].
Instead of adaptive PPF, a hybrid controller by combining μsynthesis and robust input shaping is used in this paper. $\mu $synthesis is an optimal control technique which offers the advantage of maintaining robust performance and stability by incorporating system uncertainties during controller formulation. Other advantages include possible tradeoff among stability, performance, and control energy by using suitable design weights. Also, simultaneous suppression of multiple modes and MIMO controller formulation can be easily achieved through a unified and systematic procedure. The proposed controller is used to suppress vibrations of a flexible manipulator resulting from slewing motion. The slewing motion of the manipulator is controlled by the PD controller. The model of the manipulator is taken as a flexible beam with a variable tip mass (payload). The ranges of system parameters variations are determined by developing manipulator models for a varying payload of 01 kg. This payload variation caused an uncertainty of around ±50 % in first modal frequency. Effectiveness of the proposed controller is demonstrated by comparative studies with other hybrid controllers formed by robust input shaping and PPF. Dependence of hybrid controller performance on design frequencies of input shaper is also studied. Results of comparison showed that the hybrid controllers using $\mu $controller gave better performance in terms of settling time and energy consumption than those using PPF.
The rest of the paper is as follows: mathematical modeling is described in Section 2; principle of input shaping and design of controllers are discussed in Section 3; simulation results are presented in Section 4 and finally Section 5 concludes this paper.
2. Mathematical modeling
The equation governing the dynamic response of a structure embedded with piezoelectric actuators can be expressed using finite element formulation as [1214]:
where [$M$], [$C$], [${K}_{xx}$], [${K}_{xu}$] and [${K}_{uu}$] are the, mass, damping, elastic stiffness, piezoelectric coupling and dielectric stiffness matrices, respectively; $X$ and ${F}_{m}$ denote the vectors of structural displacement degrees of freedom (D.O.F) and applied mechanical load respectively; $U$ is the vector of applied piezoelectric actuator voltages; [${K}_{m}$] is a matrix for locations of applied mechanical loads and [${T}_{a}$] is a matrix of actuator locations with corresponding capacitances.
However, the number of D.O.F, Eq. (1) are usually large and modal transformation is generally applied for obtaining reduced model for control design purposes. The transformation to modal coordinates is expressed as:
where columns of the square matrix [$\varphi $] are eigenvectors of undamped homogenous system of Eq. (1) and η represents modal coordinates. By using Eq. (2) and assuming proportional damping, Eq. (1) can be transformed in modal coordinates. The resulting equation can be expressed in abbreviated form as:
By taking the state vector as $\Omega ={\left[{\eta}^{T},{\dot{\eta}}^{T}\right]}^{T}$ and normalizing the eigenvectors in Eq. (2) with respect to mass matrix of Eq. (1), the system model in state space form can be expressed as:
where the system matrices have the following structure:
where $C$ and $\omega $ are modal damping and natural frequencies, respectively; ${B}_{1}$ and ${B}_{2}$ represent input matrices corresponding to applied mechanical loads and piezoelectric actuator inputs; and subscript $n$, ${n}_{m}$, ${n}_{a}$ denote number of modes used in transformation, number of applied mechanical loads and number of piezoelectric actuators inputs, respectively.
Outputs corresponding to sensor measurements can be represented in state space form as follows:
where subscript ${n}_{y}$ denotes the number of measured outputs; $\mathrm{\Gamma}$ is a matrix of dimension ${n}_{y}\times 2n$, which transforms modal coordinates into physical outputs; matrix ${D}_{1}$ with dimension ${n}_{y}\times {n}_{m}$ is feed through matrix for applied mechanical loads and matrix ${D}_{2}$ with dimension ${n}_{y}\times {n}_{a}$ is feed through matrix for applied actuator voltages.
Inputs corresponding to modal disturbances can be included in Eq. (4) as follows [15]:
where the vector of modal forces is represented by $\stackrel{~}{f}$ and matrix ${B}_{3}$ has the following structure:
The modal response of the system can also be obtained as follows:
With:
Use of commercial finite element software ANSYS for performing closed loop simulations as well as obtaining system model in the form represented by Eqs. (45) has been demonstrated by [1619].
In this paper system model is obtained by performing modal analysis in ANSYS for inputs: (a) input torque for controlling slewing motion, and (b) applied piezoelectric actuator voltage; and outputs corresponding to strains and tip deflection. While the inputs and outputs corresponding to modal disturbances and responses are appended to the system model by using Eqs. (67).
The model of the flexible manipulator used in this paper is shown in Fig. 1(a). The manipulator arm is modeled as 2.5 mm thick aluminum beam with material properties: $E$ (Modulus of elasticity) = 69×10^{9} N/m^{2}; $\rho $ (Density) = 2710 kg/m^{3}; $\upsilon $ (Poisson’s ratio) = 0.32. The motor assembly governing the slewing motion is modeled as a rigid hub. The control action for suppressing vibration is provided through, four DuraAct patches (P876.A15) of ©Physik Instrumente (PI) [20]. A collocated strain gauge is used for providing strain measurements. Manipulator’s dimensions along with locations of actuators and strain gauge are shown in Fig. 1(a). Material properties of piezoelectric patches are provided in Table 1.
Fig. 1. Model of manipulator
a) Sizes and locations of components
b) Corresponding FEM model of manipulator
Table 1. Material properties of piezoelectric actuators
Compliance at constant electric field (m^{2}/N)

Piezoelectric strain matrix (m/V)

Relative permittivity at constant stress

Density (kg/m^{3})

Free space permittivity (F/m)


S11

1.590×10^{}^{11}

d31

–1.74×10^{}^{10}

$\epsilon 11$

1649

7800

8.85×10^{}^{12}

S33

2.097×10^{}^{11}

d33

3.94×10^{}^{10}

$\epsilon 22$

1649


S12

–5.699×10^{}^{12}

d15

5.35×10^{}^{10}

$\epsilon 33$

1750


S13

–7.376×10^{}^{12}


S44

4.492×10^{}^{11}


S66

4.319×10^{}^{11}

The corresponding finite element model of the manipulator is shown in Fig. 1(b). The motor assembly and the tip load are modeled as concentrated masses by using “MASS 21” element. Moment of inertia of the motor assembly about rotation axis is taken as 10 kg/m^{2}. Manipulator’s arm is modeled by using “SOLID 186” element, and “SOLID 226” element is used for piezoelectric patches modeling. The “MASS 21” element (hub) and manipulator arm are connected through constraint equations. A global element size of 12.5 mm is used for meshing. The system model and variations in its parameters are obtained by performing modal analysis for 21 payload values (from 0 to 1 kg with increment of 0.05 kg). The modal analysis is performed by assuming free rotation about axis of rotation and a uniform modal damping ratio of 0.5 %. Detailed procedure for obtaining system matrices through modal analysis is available in [21].
3. Design of controllers and input shaper
The block diagram of the system with proposed hybrid controller configuration is shown in Fig. 2. The inputs, to the plant shown in Fig. 2, correspond to torque applied for slew motion and applied piezoelectric actuator voltage respectively, while the outputs correspond to rotation angle and strains respectively. The inner loop connecting the strain measurements to piezoelectric actuators’ input, via a controller (PPF or $\mu $), provides the means for active vibration suppression. The outer loop, controlled by the PD controller, is responsible for providing the slewing motion. To suppress the vibrations to manageable level, the slew command is applied to the system through an input shaper. The parameters of the input shaper are calculated for a system model with closed outer loop and open inner loop. The control action through piezoelectric actuators is started after the last shaper impulse, this is done to avoid saturation of actuators due to high initial response of the structure. The design details of each component of the configuration shown in Fig. 2 are as follows.
Fig. 2. System block diagram for hybrid controller configuration
3.1. PD controller
The slewing motion of the manipulator is controlled by PD controller. The PD controller is designed by using nominal values of system parameters. Proportional and derivative gains of the PD controller used in this paper are taken as 0.185 and 16.8 respectively.
3.2. Input shaping
The methodology by which a shaped command moves a flexible system without vibration can be explained by considering the response of an under damped flexible system to impulse inputs. Consider Fig. 3 which for the sake of simplicity shows the response of a single flexible mode to two suitably timed impulses. The total response shows no vibratory motion after the second impulse, this is achieved by cancelling the vibratory motion resulting from 1st impulse by suitably placing the 2nd impulse of appropriate amplitude. A single impulse input can be thought of as a building block of an arbitrary input, hence, properly timed impulse sequence can be used for generating arbitrary vibration reducing inputs. This is achieved by convolving any arbitrary desired input to the system with the impulse sequence called input shaper [2].
Fig. 3. Impulse response of a flexible mode for suitably timed impulses
The design of input shaper is achieved by solving the equation governing the system response to an impulse input with a set of constraints. Most types of constraints can be categorized as residual vibration constraints, robustness constraints, impulse amplitude constraints, and the requirement of time optimality. In this paper, a three impulse robust input shaper is used. The formulas for amplitude and time instances of the shaper impulses for suppression of individual mode are [22]:
where $K=\mathrm{e}\mathrm{x}\mathrm{p}((\pi \xi /\sqrt{1{\xi}^{2}}\left)\right)$, $\xi $ and ${\omega}_{d}$ are the damping ratio and damped natural frequency of the mode to be suppressed.
For simultaneous suppression of multiple modes, the final shaper can be composed by convolving the individual shapers [23]. In this paper, the shaper is designed for suppressing first two modes. As discussed earlier the parameters of individual shapers are obtained for a system model with closed outer loop and open inner loop (see Fig. 2). The shaped command designed for the nominal system model (system model developed by taking mean values of system parameter) along with unshaped input is shown in Fig. 4. The vibratory response of nominal system model at the manipulator’s tip and the response of first two modes, for the shaped and unshaped inputs are shown in Fig. 5.
Both PPF and input shaping are very effective at their design frequencies, however, both can only guarantee performance for limited variation of system parameters. Hence, for large system parameter variations, the overall effective band of hybrid controller can be increased by placing design frequencies of PPF and input shaper apart. Motivated by this fact the PPF controller in this paper is designed for nominal system parameters while the design frequencies of input shaper are varied in order to constitute the most effective hybrid controller. Hybrid controllers formed by combining these shapers with PPF or $\mu $ controllers are discussed in section hybrid controller formulation.
Fig. 4. Slew angle command to the system
3.3. PPF controller design
PPF is basically a second order compensator which operates on generalized position output of the structure for generating a force command that is used for suppressing vibration. Due to ease of implementation and high immunity to spillover under collocated actuator/sensor condition, it has been widely used for suppressing vibration of flexible structures [12, 2436]. Basic structure of the PPF controller when applied for single mode control is shown in Fig. 6.
The design of a PPF controller is based on its three parameters: damping (${\xi}_{c}$), frequency (${\omega}_{c}$), and gain ($K$). Guidelines for selecting these parameters have been given in number of studies [24, 32, 35, 36]. In this paper, optimal parameters of the PPF controllers are determined by using analytically derived formulas given by [24].
Fig. 5. Nominal system response at manipulator’s tip
a) Total
b) 1st mode
c) 2nd mode
The PPF controller in this paper has been designed for nominal system parameters. The parameters of the designed PPF controllers are given in Table 2.
Table 2. Design parameters for PPF controllers
Design parameter

Mode 1

Mode 2

$K$

2.5603e+006

173.0971

${\omega}_{c}$

8.7092

55.2087

${\xi}_{c}$

0.273

0.007

Fig. 6. PPF control structure
Fig. 7. Basic framework for $\mu $control synthesis
3.4. $\mathit{\mu}$controller design
The general framework for the $\mu $controller design is shown in Fig. 7 Where $\mathrm{\Delta}$ is norm bounded perturbation which describes the uncertainty structure; $P$ is the open loop interconnection which includes all the scaling and weighting functions used to describe these perturbations, input disturbances, and performance measures; input vector $d$ represents external disturbances to the system; output vector $e$ is used to represent performance measures; and $K$ is the controller. By using linear fractional transformation any linear interconnection of inputs and outputs along with associated uncertainties and controller can be rearranged to match this framework [37].
Detailed system model used for control formulation in this paper is shown in Fig. 8. Since for the considered manipulator model the vibratory response is dominated by the first two modes, a reduced two mode plant model is used for inbandwidth plant modeling. This reduction of plant model is necessary to keep the order of designed controller reasonable.
Also, to independently control the amount of damping added to each mode, system inputs/outputs corresponding to input torque/tip deflection have been replaced by modal disturbances/modal responses. Independent control of amount of damping is particularly suitable for the type of system considered in this paper, where the amount of damping required for achieving a desired settling time also depends on modal frequency (a mode with higher modal frequency requires less damping for achieving a desired settling time). To keep the actuators effort in reasonable limits a performance output corresponding to controller’s output signal has also been included in the system’s description. The objective is to ensure desired modal damping, in presence of plant uncertainties and control signal limitations, while keeping the system robustly stable. For $\mu $ control synthesis this objective has to be represented in terms of infinite norm of the system. Moreover, for meaningful representation of this objective, weights (also shown in Fig. 8) are used for scaling system’s inputs and outputs [38, 39]. The uncertainties considered in this paper for control formulation are due to: (a) variation in system natural frequencies caused by change in payload, and (b) exclusion of higher order system modes from system model. The uncertainty in system matrix due to variation in natural frequencies is modeled as real parametric uncertainty as follows:
where, ${\delta}_{i}$ represents the percentage uncertainty in term ${\omega}_{i}^{2}$ (square of the ith modal frequency). Using linear fractional transformation this uncertainty is represented as a 2×2 diagonal block structure ${\u2206}_{st}=\left[\begin{array}{cc}{\delta}_{1}& \\ & {\delta}_{2}\end{array}\right]$ in feedback with the reduced plant model (Fig. 8) [37, 39]. Effect of unmodeled modes is included as complex dynamic uncertainty (${W}_{bound}{\u2206}_{ad}$ Fig. 8) [40]. Where ${W}_{bound}$ represents the bound on magnitude of unmodeled higher modes and ${\u2206}_{ad}$ is a 1×1complex uncertainty block. Fig. 9 shows 20 random samples of the inbandwidth model, 20 random samples of the unmodeled system, worst gain of the unmodeled system as a function of frequency and the envelop (${W}_{bound}$) used for complex dynamic uncertainty.
Fig. 8. Modified system block diagram with modified inputs/outputs and associated weights for $\mu $control synthesis
As a general guideline, the weights used for scaling input (${W}_{dist}$) can be chosen to represent the respective magnitude of exogenous influences as a function of frequency and the weights used for scaling outputs (${W}_{mod}$, ${W}_{act}$) are chosen as inverse of the bound on desired respective output [38]. Since, a two mode model is used for inbandwidth modeling, ${W}_{dist}$ and ${W}_{perf}$ are taken as 2×2 diagonal matrices; where each diagonal entry correspond to the weight selected for the corresponding mode. After performing some trial and error the nominal values of weights selected for controller design are summarized in Table 3.
Table 3. Nominal weight values for $\mu $ controller
Design parameters/ weights

Nominal values

${W}_{dist}$

$\left[\begin{array}{cc}0.058& \\ & 1.3817\end{array}\right]$

${W}_{mod}$

$\left[\begin{array}{cc}9.711& \\ & 15.56\end{array}\right]$

${W}_{act}$

0.0045

Fig. 9. Uncertain system response and bound for residual system
Fig. 10. Frequency response of weights used for penalizing system inputs and outputs
a) Modal response weight
b) Modal disturbance weights
The above nominal values of weights have been calculated to provide desired amount of damping for the $i$th mode at its nominal frequency. For a system with uncertain modal frequencies, the worst response of a mode decreases at 20 dB/decade within its uncertainty band. Hence, for maintaining a constant value of desired closedloop damping in the uncertainty band, the weight ${W}_{{mod}_{i}}$ (weight for the ith mode) has to be varied accordingly. Fig. 10(a) shows the uncertain modal response $Gi$ (response of the $i$th mode from $i$th modal disturbance to $i$th modal output) along with typical variation of $1/{W}_{{mod}_{i}}$ that can be used for this purpose. Where, at the $i$th nominal frequency, the magnitude of frequency dependent ${W}_{{mod}_{i}}$ should be made equal to the nominal ${W}_{{mod}_{i}}$ obtained above.
Also, to limit the band of modal disturbances, variation of ${W}_{{dist}_{i}}$ shown in Fig. 10(b) can be used. Where the magnitude of frequency dependent ${W}_{{dist}_{i}}$, at the $i$th^{}nominal frequency, should be made equal to the nominal ${W}_{{dist}_{i}}$ obtained above. In this paper frequency variations, similar to those shown in Fig. 10 have been adopted for $1/{W}_{{mod}_{i}}$ and ${W}_{{dist}_{i}}$ respectively.
The controller is designed by using mixed $\mu $synthesis [3739]. Afterwards, the order of the controller is reduced to 7 by applying “Balanced model truncation via square root method” [38, 41].
3.5. Hybrid controller formulation
The hybrid controllers are formed by combining PPF or $\mu $ controllers with input shapers designed for system parameters corresponding to payloads values from 0 to 1 kg with increment of 0.05 kg. The design of input shaper for different values of payloads is done to determine the design parameters of the shaper resulting in most effective hybrid controller. In this paper input shaper designed for system frequencies corresponding to 0.65 kg payload resulted in best hybrid control performance. In order to show the effect of input shaper design frequencies on hybrid controller performance, the results of hybrid controllers with input shapers designed for: (a) nominal system parameters, (b) lowest possible frequencies of each mode, and (c) system parameters corresponding to 0.65 kg payload are presented in next section.
4. Results
A total of eight control configurations have been evaluated in this paper, out of these eight configurations six are hybrid which are formed by combining input shapers with PPF or $\mu $ controllers. Details of the parameters used for designing these configurations are summarized in Table 4.
For evaluating the performance of control configurations listed in Table 4, a step command of 5 degree slew angle is given to the manipulator. The performance is evaluated in terms of the settling time required for reducing manipulator’s tip vibration to 1 % of its maximum amplitude in openloop condition with a 0.5 kg payload. For each control configuration 21 simulations are performed by varying the payload from 0 to 1 kg in steps of 0.05 kg. The required settling time and the power consumed by the active vibration controller ($\mu $ or PPF) are recorded for each simulation. The results of the simulations are summarized in terms of four comparative studies as follows.
Table 4. Parameters for control configurations
Controller

System parameters used for designing input shaper (IS)

System parameters used for designing controller for vibration suppression

PPF

–

Nominal system parameters

$\mu $

–

Uncertainty range of system parameters

IS nom + PPF

Nominal frequency of each mode

Nominal system parameters

IS low + PPF

Lowest frequency within uncertainty range of each mode

Nominal system parameters

IS 0.65kg + PPF

System parameters corresponding to 0.65 kg payload

Nominal system parameters

IS nom + $\mu $

Nominal frequency of each mode

Uncertainty range of system parameters

IS low + $\mu $

Lowest frequency within uncertainty range of each mode

Uncertainty range of system parameters

IS 0.65 kg + $\mu $

System parameters corresponding to 0.65 kg payload

Uncertainty range of system parameters

4.1. Case A and B
In case A, the results of $\mu $ and PPF controller are compared. The resulting settling for the 21 simulations are shown in Fig. 11(a). In case B, the same controllers are combined with the input shaper designed for nominal system frequencies. Simulation results for case B are shown in Fig. 11(b). As can be seen from Fig. 11, although the $\mu $ controller configurations performed better than their counterpart PPF configurations the control action for all configurations become ineffective at high payload. One reason for this, is the decrease in system natural frequencies due to increase in payload (motion at high frequency requires less damping for achieving a desired settling time). To overcome this problem the input shaper for case C is designed by using the lowest frequencies within the uncertainty range of each mode.
Fig. 11. Settling time required for $\mu $ and PPF controllers
a) Without input shaping
b) With input shaping (shaper designed for nominal system frequencies)
4.2. Case C and D
The settling times required for $\mu $, and PPF controllers when combined with input shaper designed using lowest frequencies within the uncertainty range of each mode are shown in Fig. 12(a). The markedly improve results of Fig. 12(a) clearly show the advantage of judiciously choosing the design frequencies of input shaper. Moreover, as in the previous cases the μ controller configurations outperformed their counterpart PPF configurations. To explore the possibility of further improved results the design frequencies of the input shaper are varied, the best results are obtained with input shaper designed for system frequencies corresponding to 0.65 kg payload. These results are shown in Fig. 12(b). Again the $\mu $ controller configuration resulted in much better worst settling time as compared with the PPF controller configuration.
Fig. 12. Settling time required for $\mu $ and PPF controllers
a) With input shaper designed for lowest frequency of each mode
b) With input shaper designed for system parameters corresponding to 0.65 kg payload
Table 5. Ratios of power consumed by PPF and $\mu $ controllers
Case

Consumed power ratio ($\mu $/PPF)

Case A: PPF VS $\mu $

0.67

Case B: IS nom + PPF VS IS nom + $\mu $

0.74

Case C: IS low + PPF VS IS low + $\mu $

0.78

Case D: IS 0.65 kg + PPF VS IS 0.65kg + $\mu $

0.99

The ratios of the power consumed by the $\mu $ controller to the PPF controllers for all the above cases are given in Table 5. As can be seen in all cases $\mu $ controller configurations also resulted in lower power consumption as compared to the respective PPF controller configurations.
4.3. Stability characteristics
The stability characteristics of the whole control system, consisting of both inner (controlled by PD controller) and outer (controlled by PPF or $\mu $ controller) loops are determined by assuming simultaneous independent gain and phase variation in each loop. The multiloop disk gain and phase margin calculated by using balanced sensitivity function [38, 42], for system models corresponding to payload variation of 01 kg are shown in Fig. 13. For the considered system models $\mu $ controller also resulted in better stability characteristics of the system.
Fig. 13. Multiloop disk margins
a) Gain margin
b) Phase margin
5. Conclusions
Results of hybrid vibration controllers, applied for vibration suppression of an uncertain model of flexible manipulator, are presented in this paper. The proposed hybrid controller combines robust input shaping for command input with $\mu $controller applied for active vibration suppression using smart materials. Results of comparative studies of the proposed controller with hybrid controllers formed by PPF and input shaping showed, better settling time and power consumption for $\mu $controllers. Also for the considered system $\mu $ controller resulted in better stability characteristics of the system. Moreover, it is shown that that the performance of hybrid controller is strongly dependent on the parameters used for designing input shaper, and the effectiveness of the hybrid controller can be substantially increased by judiciously selecting the design frequencies of input shaper.
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