An aircraft A is flying in a vertical plane containing two tracking stations P and Q which are 15km apart. At a cetain instant θ (measured anticlockqise from horizontal line PQ to the line PA) is 60° and the $ \dot \theta $ (angular velocity) is -0.025rad/s. At the same time, α (measured anticlockqise from extended horizontal line PQ to the line QA) is 150° and the $\dot \alpha$ is -0.02rad/s. Determine the magnitude and the direction of the velocity of the aircraft.
I used the radial and transverse components of the velocities relative to P and Q and calculated the resultant.
Relative to P, radial component = $$\frac{d(PA)}{dt}= \frac{d(15000Cos(\theta))}{dt} = -15000Sin(\theta) \dot \theta $$
The transverse component = $$r \dot \theta =-(PA)0.025$$
The components of velocity relative to Q could be obtained in the same way but I'm not sure about what to do next. Is taking the resultant of them correct? I took the resultant and got the following answers.
Magnitude - 15133m/s
Direction - 88.89° north of east
$$OA = OPtan(\theta)$$ $$d(OA) = d(OP)tan(\theta) + OPsec^{2}(\theta)d\theta ......(1)$$
Similarly,
$$OA = OQtan(\alpha)$$ $$d(OA) = d(OQ)tan(\alpha) + OQsec^{2}(\alpha)d\alpha ........(2)$$
OQ = 15000-OP
$$\frac{OA}{OP} = tan(60)$$
$$\frac{OA}{OQ} = tan(30) = \frac{OA}{15-OP} = tan(30)$$
Solving these two : You will find that $OP = 3.75$$
$$ \frac{d(OA)}{dt} = \frac{d(OP)}{dt}tan(\theta) +OPsec^{2}(\theta)\frac{d\theta}{dt}...(3)$$ $$ \frac{d(OA)}{dt} = \frac{d(OQ)}{dt}tan(\alpha)+ OQsec^{2}(\alpha)\frac{d\alpha}{dt}.....(4)$$
$$\frac{d\theta}{dt} = \theta^{o}$$ $$\frac{d\alpha}{dt} = \alpha^{o}$$
Substituting the values of $\theta, \alpha,\theta^{o},\alpha^{o}, OP, OQ$,
we get, and solving (3) and (4) we get the y component $\frac{d(OA)}{dt} $ and the x component $\frac{d(OP)}{dt}$ and take the magnitude $\sqrt{x^2+y^2}$ou will get
$$ v = 320$$m/sec and the angle will be the $tan^{-}(\frac{y}{x}) = 23.9$ degrees.