An aircraft can maintain a speed of 300km h−1 relative to still air. A wind of 80km h−1 is blowing from the south-west (that is, from 225∘ measured clockwise from the north). The pilot wishes the resultant ground track of the aircraft to be due north.
a. (i) Express the wind velocity vector in terms of eastward i and northward j components.
b. (ii) Let the aircraft head be at an angle θ east of north. Write the velocity of the aircraft relative to the air in component form in terms of θ.
c. (iii) Using vector addition, find the value of θ (to the nearest 0.1∘) that will ensure a due-north ground track, and compute the corresponding ground speed of the aircraft.