testing the volatility and leverage feedback hypotheses using garch(1,1) and var models
DESCRIPTION
The returns of the Boeing company are used in the estimation of a GARCH(1,1), and consequently, a Vector Autoregressive model, which are then utilized for testing the leverage and volatility feedback effect hypotheses of the company's share prices.TRANSCRIPT
Contents
Contents 2
List of Figures 3
List of Tables 4
1 Testing Nonstationarity 5
2 Volatility Estimation 6
3 VAR Estimation 8
4 Testing Leverage and Volatility Feedback Effects 9
References 22
2
List of Figures
1 The Natural Logarithm of Boeing’s Adjusted Closing Share Prices 11
2 First Differences Plot of the Natural Logarithm of the Share Prices 11
3 SACF of ln(S) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
4 SACF of the First Differences . . . . . . . . . . . . . . . . . . . . 12
5 SPACF of the First Differences . . . . . . . . . . . . . . . . . . . 14
6 Normality Test of GARCH(1,1) Residuals . . . . . . . . . . . . . 16
7 Plot of the Conditional Variance Estimated by GARCH(1,1) . . . 17
8 Correlogram of VAR(5) Residuals . . . . . . . . . . . . . . . . . . 19
9 Impulse Responses . . . . . . . . . . . . . . . . . . . . . . . . . 20
3
List of Tables
1 Coefficients measured by the ADF test . . . . . . . . . . . . . . . 13
2 The ADF Unit Root Test for the Share Prices . . . . . . . . . . . 13
3 The ADF Unit Root Test for the First Differences . . . . . . . . . 13
4 AIC for Different ARMA Orders . . . . . . . . . . . . . . . . . . . 14
5 ARMA(5,3) Model . . . . . . . . . . . . . . . . . . . . . . . . . . 15
6 Testing ARCH Effect . . . . . . . . . . . . . . . . . . . . . . . . . 16
7 Estimated VAR Model (Coefficients marked with asterisks are
Significant at 5%) . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
8 VAR(5) Residual Correlation Matrix . . . . . . . . . . . . . . . . . 18
9 Multivariate Normaility Test of VAR(5) Residuals . . . . . . . . . 20
10 Granger Causality Analysis . . . . . . . . . . . . . . . . . . . . . 21
4
1 Testing Nonstationarity
The adjusted closing share prices of Boeing have been retrieved from Yahoo
Finance for the past five years. The ln plot of the aforementioned time-series is
shown in Figure 1.
The ln(S) process appears to violate the conditions of constant mean and con-
ditional variance of weak stationarity. The first differences plot in figure 2, further
reveals that the process may be first-order integrated. These findings are con-
firmed by the slow decaying SACF plot (fig. 3) of the ln(s) process, which unlike
∆ln(s) (fig. 4) shows the high correlation of the process with its own lags.
Graphical means of testing nonstationarity may be deceiving. A plausible
approach for testing nonstationarity is to start from a general relationship such
as equation (1), which includes an intercept, an autoregressive process of order
p and a time trend, and by conducting appropriate tests (e.g. Perron Sequential
Testing Procedure) simplify to one of the cases of nonstationarity: No drift or no
trend, drift but no trend, both drift and trend.
ln(St) = α + δt+ θln(St−1) +
p−1∑j=1
pj∆ln(St−j) + ut (1)
Dougherty (2011) suggested that the aforementioned general-to-specific ap-
proaches have low power that may lead to ambiguity. A pragmatic approach
for choosing an appropriate Dickey-Fuller test is to analyse the plot of the data
and look for obvious trends.
Evidently, the data has an upward trend. Hence, the appropriate choice of a
Dickey-Fuller test includes a drift and a deterministic trend.
The unit root null hypothesis is
H0 : θ = 1 (2)
against the alternative
HA : |θ| < 1 (3)
5
The number of lags of the ADF test is chosen by Eviews using the Schwarz
Information Criterion to minimize
SIC = log(RSS
T) +
klogT
T= log(
RSS
T) +
(p+ 2)logT
T(4)
Surprisingly, the ADF test chose 0 lags for the model. Furthermore, as shown
in table 1, the trend and the constant coefficients are highly significant, which
implies the correct choice of the model.
Since the ADF t-statistic in table 2 is not larger in absolute terms than the critical
values of DF with a trend and a constant, the unit root null hypothesis does not
get rejected. Taking the first-differences and conducting the ADF test with no
intercept and no trend yields the t-statistic in table 3, indicating the stationarity
of the data and integration of first order.
2 Volatility Estimation
To estimate the volatility of the share prices, initially an appropriate ARMA model
is chosen. The first differences plot and the unit testing procedure carried out
earlier, indicate that the process is first order integrated and the returns are sta-
tionary. To choose an appropriate ARMA model, the Box-Jenkins approach is
utilised.
The order of the model is determined by choosing the number of parameters
that minimizes the information criterion and yields a parsimonious model. Infor-
mation criterion models are functions of RSS, and penalise adding extra param-
eters. In this case AIC is chosen, which overparameterizes, but produces better
results in practice (Dougherty, 2011).
The SACF and SPACF of the returns (fig. 4 & 5) do not possess any of the
AR and MA ‘signatures’ and are of little help. The information criterion is min-
imised with an ARMA(4,5) model (Table 4). However, the joint-null hypothesis
6
of no autocorrelation gets rejected at 5% level of significance for numerous lags
when diagnosing residuals using Ljung-Box Q-statistic; hence, the next best
model of ARMA(5,3) is chosen, which does not suffer from this issue.
Rt = c+5∑
i=1
φiyt−i +3∑
j=1
θjut−j + ut (5)
Once the ARMA model is determined, the ARCH effect with 5 lags is analysed.
Both the LM-statistic and F-statistics in table 6 are highly significant, suggesting
the existence of ARCH in R and persistence in the variance of returns.
The GARCH(1,1) is estimated
ht = 1.26× 10−5
(4.39)+ 0.097u2t−1
(6.63)
+ 0.846ht−1(38.22)
(6)
All coefficients are highly significant, and the analysis of the correlogram
and Ljung-box Q-statistic at the 36th lag is 36.045 with p-value of 0.14, sug-
gesting that the autocorrelation of squared residuals of the mean (i.e. ARCH
effect) has been captured by the GARCH(1,1) model. The Jarque-Bera test in
figure 6, rejects the null hypothesis of normality of the residuals. Therefore, the
GARCH(1,1) model is estimated again using Robust Standard Errors to obtain
unbiased estimators
ht = 1.10× 10−5
(2.78)+ 0.087u2t−1
(4.29)
+ 0.862ht−1(27.42)
(7)
The graph of the conditional volatility estimated by the model is shown in fig-
ure 7. The sum of the squared residual and variance coefficients in GARCH(1,1)
is 0.95, showing the high persistent (close to 1), yet mean reverting nature of
the volatility model.
7
3 VAR Estimation
For estimating VAR, it is important that the variables are stationary or cointe-
grated. Thus far, our analysis has indicated that both returns and the estimated
volatilities are stationary. Hence, testing cointegration is not necessary, as the
processes do not possess unit roots.
To select the optimal order of the VAR model, such that the errors follow a white
noise process, the objective is to minimise the information criterion, which in
this case is accomplished by choosing a lag of 5 based on MAIC. It is evident
that not all coefficients are statistically significant (table 7). However, before
analysing the estimated model and making conclusions based on t-statistics,
the assumptions of VAR(p) are checked to ensure that the OLS estimation of
the equation is consistent, efficient and approximately normal.
Since the dependent variables are stationary, the no autocorrelation assump-
tion of the error terms is expected to hold. Figure 8 indicates that there is no
substantial autocorrelation. This is consistent with the autocorrelation LM-test
at 5% significance level, which fails to reject the null hypothesis of no autocor-
relation at almost all lags, and the residual correlation matrix in table 8.
Finally, a multivariate normality test with χ2 statistics associated with skewness
and kurtosis in table 9, shows that the error terms are not normally distributed.
Furthermore, the homoscedasticity null hypothesis gets rejected at 5% signifi-
cance with a χ2 statistic of 1171. Nevertheless, according to Sims et al (1990),
the use of t-tests and F-tests is appropriate when the coefficients of interest are
stationary, and given a large sample size, the critical values of a normal distri-
bution may be used.
To interpret the estimated model, impulse responses have been constructed
to analyse the responsiveness of the dependent variables to unit shocks to the
8
error terms. Due to the stationarity of the return and volatility variables, the
estimated VAR is stable and mean-reverting. As expected, figure 9 shows that
the shock effects fade away over time. The highest persistent shock is the
impact of a unit shock to volatility on volatility itself. Furthermore, a unit shock
to the returns leads to an inverse shift in volatility. The impact of a shock to
volatility is small on returns, while a unit shock to the return has a large impact
on returns itself; though the effect fades away exponentially.
4 Testing Leverage and Volatility Feedback Effects
To test whether leverage and volatility feedback effects are present, we wish to
test the null hypotheses
H0 : No volatility feedback effect (8)
H0 : No leverage effect (9)
“The fundamental difference between the leverage and volatility feedback expla-
nations lies in the ‘causality’: the leverage effect explains why a negative return
leads to higher subsequent volatility, whereas the volatility feedback effect justi-
fies how an increase in volatility may result in negative returns”.(Bollerslev et al,
2006)
In earlier section, a VAR(5) model was estimated in which returns and volatilities
are endogenous variables with impacts on one another. The model is
Rt = c+5∑
j=1
αjRt−j +5∑
j=1
βjht−j + ut (10)
ht = c+5∑
j=1
γjht−j +5∑
j=1
δjRt−j + ut (11)
9
To test whether the returns have any significant impact on volatility and vice
versa, the Granger Causality test conducts a joint hypothesis using an F-test
H0 : β1 = β2 = ... = βj = 0 for equation 10 (12)
and
H0 : δ1 = δ2 = ... = δj = 0 for equation 11 (13)
Null-hypothesis (12) does not get rejected (table 10), which implies there is no
volatility feedback effect. The second F-statistic on the other hand is highly
significant, which indicates that returns have a significant impact on volatility.
Furthermore, figure 9 shows that this relationship is inverse, rejecting the no
leverage effect hypothesis.
10
Figure 1: The Natural Logarithm of Boeing’s Adjusted Closing Share Prices
Figure 2: First Differences Plot of the Natural Logarithm of the Share Prices11
Variable Coefficient Std Error t-statistic
α 0.034 0.13 2.53
t 0.00000841 0.00000303 2.78
Table 1: Coefficients measured by the ADF test
t-statistic
ADF Test-Statistic -2.54
Critical Values of the Test 1% -3.97
5% -3.41
-3.13
Table 2: The ADF Unit Root Test for the Share Prices
t-statistic
ADF Test-Statistic -34.50
Critical Values of the Test 1% -3.97
5% -3.41
10% -3.13
Table 3: The ADF Unit Root Test for the First Differences
13
Figure 5: SPACF of the First Differences
ARMA(p,q) q=1 q=2 q=3 q=4 q=5
p=1 -5.5347 -5.5375 -5.5366 -5.5354 -5.5347
p=2 -5.5371 -5.5474 -5.5463 -5.5452 -5.5342
p=3 -5.5356 -5.5359 -5.4782 -5.5465 -5.5322
p=4 -5.5347 -5.5354 -5.5474 -5.5497 -5.5513
p=5 -5.5347 -5.533 -5.5469 -5.5502 -5.5499
Table 4: AIC for Different ARMA Orders
14
Vari
able
cA
R(1
)A
R(2
)A
R(3
)A
R(4
)A
R(5
)M
A(1
)M
A(2
)M
A(3
)
Coe
ffici
ent
0.00
071.
6969
*-1
.594
9*0.
5586
*-0
.002
2-0
.040
2-1
.684
6*1.
5547
*-0
.54*
Std
.Err
or0.
0004
0.22
530.
2655
0.23
430.
0612
0.03
430.
2246
0.25
650.
2057
t-st
atis
tic1.
847.
53-6
.00
2.38
-0.0
3-1
.16
-7.4
96.
06-2
.62
Pro
b(F-
stat
)0.
0001
75
Tabl
e5:
AR
MA
(5,3
)Mod
el
15
Test-Statistic Coefficient p-values
F-Statistic 30.738 0.0000
LM-Test 137.427 0.0000
Table 6: Testing ARCH Effect
Figure 6: Normality Test of GARCH(1,1) Residuals
16
ht Rt
c 1.32× 10−5∗ 0.000131
(5.86) (0.153)
ht−1 0.984134∗ −11.63049
(34.81) (−1.08)
ht−2 0.064391 34.13301∗
(1.63) (2.27)
ht−3 −0.165896∗ −32.93824∗
(−4.24) (−2.21)
ht−4 0.132047∗ 13.25747
(3.36) (0.89)
ht−5 −0.069701∗ 0.033311
(−2.50) (0.00314)
Rt−1 −0.000452∗ 0.024692
(−6.058) (0.87)
Rt−2 −7.92× 10−5 −0.031109
(−1.05) (−1.082)
Rt−3 −0.000408∗ −0.026362
(−5.39) (−0.918)
Rt−4 −6.21× 10−5 −0.044414
(−0.82) (−1.54)
Rt−5 −0.000187∗ −0.059401∗
(−2.45) (−2.05)
Table 7: Estimated VAR Model (Coefficients marked with asterisks are Signifi-
cant at 5%)
h r
h 1.00 0.00278
r 0.00278 1.00
Table 8: VAR(5) Residual Correlation Matrix
18
Component Skewness Chi-sq df p-value
1 4.04 3399.205 1 0.0000
2 -0.25 13.06 1 0.0003
Joint 3412.26 2 0.0000
Component Kurtosis Chi-sq df p-value
1 27.71 31750.60 1 0.0000
2 5.34 284.17 1 0.0000
Joint 32034.77 2 0.0000
Table 9: Multivariate Normaility Test of VAR(5) Residuals
Figure 9: Impulse Responses
20
Null Hypothesis F-Statistic p-value
Volatility Does not Granger Cause Return 1.57 0.1644
Return Does not Granger Cause Volatility 13.97 0.0000
Table 10: Granger Causality Analysis
21
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22