Baby weights, Part I. (9.1, p. 350) The Child Health and Development Studies investigate a range of topics. One study considered all pregnancies between 1960 and 1967 among women in the Kaiser Foundation Health Plan in the San Francisco East Bay area. Here, we study the relationship between smoking and weight of the baby. The variable smoke is coded 1 if the mother is a smoker, and 0 if not. The summary table below shows the results of a linear regression model for predicting the average birth weight of babies, measured in ounces, based on the smoking status of the mother.
The variability within the smokers and non-smokers are about equal and the distributions are symmetric. With these conditions satisfied, it is reasonable to apply the model. (Note that we don’t need to check linearity since the predictor has only two levels.)
Average Birth weight = -8.94*Smoker + 123.05
The negative coefficient means that if a mother smokes her baby’s birth weight will be 8.94 units below the average.
Very low p value and a large coefficient lead me to believe that indeed there is a relationship
Absenteeism, Part I. (9.4, p. 352) Researchers interested in the relationship between absenteeism from school and certain demographic characteristics of children collected data from 146 randomly sampled students in rural New South Wales, Australia, in a particular school year. Below are three observations from this data set.
The summary table below shows the results of a linear regression model for predicting the average number of days absent based on ethnic background (eth: 0 - aboriginal, 1 - not aboriginal), sex (sex: 0 - female, 1 - male), and learner status (lrn: 0 - average learner, 1 - slow learner).
days absent = 2.15 x kind of learner + 3.1 x sex -9.11 x ethnicity + 18.93
lrn: days absentee of slow learners is 2.15 higer than average learners
sex: male students absentees are 3.10 higher than female students.
eth: non aboriginal students have absentees 9.11 lower than aboriginal students.
pred <- 2.15*1 +3.1*1 -9.11*0 + 18.93
#residual = actual - pred
2-pred
## [1] -22.18
#r2 = 1-(Residual Variance/ Sample variance)
r2 <- 1-(240.57/264.17)
r2
## [1] 0.08933641
Adjusted r2= 1-r2) *(n-1)/(n-k-1)
= .07009704
Absenteeism, Part II. (9.8, p. 357) Exercise above considers a model that predicts the number of days absent using three predictors: ethnic background (eth), gender (sex), and learner status (lrn). The table below shows the adjusted R-squared for the model as well as adjusted R-squared values for all models we evaluate in the first step of the backwards elimination process.
Which, if any, variable should be removed from the model first?
The highest R2 is from the model that does not have learner status in it . As such the first variable I would drop would be learner status
Challenger disaster, Part I. (9.16, p. 380) On January 28, 1986, a routine launch was anticipated for the Challenger space shuttle. Seventy-three seconds into the flight, disaster happened: the shuttle broke apart, killing all seven crew members on board. An investigation into the cause of the disaster focused on a critical seal called an O-ring, and it is believed that damage to these O-rings during a shuttle launch may be related to the ambient temperature during the launch. The table below summarizes observational data on O-rings for 23 shuttle missions, where the mission order is based on the temperature at the time of the launch. Temp gives the temperature in Fahrenheit, Damaged represents the number of damaged O-rings, and Undamaged represents the number of O-rings that were not damaged.
More O ring failures seem to occur during lower temperatures
Intercept: probabilities of damaged to undamaged o-rings is exp 11.6630 when T = 0F
Slope: m for every 10F above zero, the probability of orings failing is decreases by 0.2162
ln(Probability of failure/1-Probability of failure/) = 11.6630 - .2162 * Temperature
P value is extremly low , using a CI of 95% this makes the model statistically significant. As a result yes there is cause to worry because the probabilty of failure increases exponentially based on temperature
Challenger disaster, Part II. (9.18, p. 381) Exercise above introduced us to O-rings that were identified as a plausible explanation for the breakup of the Challenger space shuttle 73 seconds into takeoff in 1986. The investigation found that the ambient temperature at the time of the shuttle launch was closely related to the damage of O-rings, which are a critical component of the shuttle. See this earlier exercise if you would like to browse the original data.
\begin{center} \end{center}
where \(\hat{p}\) is the model-estimated probability that an O-ring will become damaged. Use the model to calculate the probability that an O-ring will become damaged at each of the following ambient temperatures: 51, 53, and 55 degrees Fahrenheit. The model-estimated probabilities for several additional ambient temperatures are provided below, where subscripts indicate the temperature:
\[\begin{align*} &\hat{p}_{57} = 0.341 && \hat{p}_{59} = 0.251 && \hat{p}_{61} = 0.179 && \hat{p}_{63} = 0.124 \\ &\hat{p}_{65} = 0.084 && \hat{p}_{67} = 0.056 && \hat{p}_{69} = 0.037 && \hat{p}_{71} = 0.024 \end{align*}\]
#p51
exp(11.663-0.2162*51)/(1+exp(11.663-0.2162*51))
## [1] 0.6540297
#p53
exp(11.663-0.2162*53)/(1+exp(11.663-0.2162*53))
## [1] 0.5509228
#p55
exp(11.663-0.2162*55)/(1+exp(11.663-0.2162*55))
## [1] 0.4432456
temperature <- c(49:76)
probability <- round(exp(11.6630-(0.2162 * temperature)) / (1 + exp(11.6630-(0.2162 * temperature))), 2)
plot(temperature, probability, type = "l", main = "O-ring Logistic curve")
The assumption is that residuals are independent. My only concern here would be the rate of O ring failures. Looking at the tables above, 5 O rings failed at 53F . tThis indicates that there might be a cutoff temperature after which the failure rate increases exponentially. If true the residuals would not be independent.