ro-pressure specific heat of dry air cp in kJ/(kg K) is given by: cp = 0.99403 + 1.671 × 10−4T + 9.7215 × 10−8T 2 −9.5838 × 10−11T 3 + 1.9520 × 10−14T 4 Here T is absolute temperature in K. Write a MATLAB script (a) to plot cp versus T  in the range between 0 to 1500 K, and                               (b) to determine the temperature that corresponds to a specific heat of 1.1 kJ/(kg K) with MATLAB polynomial functions. NOTE: 1. Axis titles and units are compulsory

I need help with programming in MATLAB. If we have a repeating ground-track orbit whose period of repetition is two orbits per day (ω⊕ = 7.2921151467 · 10−5 rad/s), has a semi-major axis of 3096.7363, an eccentricity of 0.74, an inclination of 63.4349 deg, a right ascension of the ascending node of −86.915798 deg, and argument of perigee of 270 deg. Provide the following results using 100 points equally distributed in time over an orbital period with a starting position of true anomaly equal to 0 degrees:  We are interested in studying the coverage that the orbits provide to a building (40.43094◦ N, 86.915798◦ W). The satellite has a field of view of a complete cone angle of 10 degrees pointing at Nadir. The greenwich meridian points to the aries point. Determine the ground-track of the orbit. Represent that ground-track in a 2D plotin longitude and latitude and include, with a different colour, the positionof the building in the same plot.

Please use matlab

I need help with programming in MATLAB. The following code transforms cartesian coordinates to the kepler elements. Can you give me the code for transforming kepler orbital elements to cartesian coordinates. The following code gives the 6 kepler elements. Transform those elements into cartesian coordinate that match the values under the Example Usage part of the code. Can you send a screenshot so I know the output of your code matches the input of the following code? I have asked this question twice and I have gotten the exact same code as the answer and it did not match. Please make sure the results match.   % Example usage:x = 1000;   y = 2000;   z = 3000;   vx = 4;     vy = -3;    vz = 2;      [a, ecc, inc, raan, argp, f] = cart2orb(x, y, z, vx, vy, vz); % Display the resultsdisp(['Semi-Major Axis (a): ', num2str(a), ' km']);disp(['Eccentricity (ecc): ', num2str(ecc)]);disp(['Inclination (inc): ', num2str(inc), ' degrees']);disp(['Right Ascension of Ascending Node (raan): ',…

Q3: Write a matlab program call matq3.m that returns the plot of the 2- D space defined by the following equation: (-xsin(x) cos (x) - 2π ≤ x < 0 x ≥ 2π Label the x-axis and y-axis and z-axis and title to the curve. y =

in python with a print statment

For all MATLAB programs you must include MATLAB code and the output from the program

Given the law of cosines, "A" = 60 degrees, "a" = 5 meters, and "c" = 2 meters. How can I write a program in MATLAB to solve for the equation and value of "b" using the syms, double, and subs command

Write a matlab program that computes the values of this function: Dn = 6 +((n -1) - ((6(n+1))/n) where the value of n is entered by the user and displayed with headings