function [A] = getTestData(epoch_secs)
A = NaN(1,108);
secondsbytes =  typecast(cast(epoch_secs,'uint32'),'uint8');
A(5:8) = secondsbytes(4:-1:1);
%Angles
A(9)  = uint8(hex2dec('00'));
A(10) = uint8(hex2dec('1b'));
A(11) = uint8(hex2dec('ff'));
A(12) = uint8(hex2dec('fd'));
A(13) = uint8(hex2dec('3a'));
A(14) = uint8(hex2dec('5b'));
        
%Angular Rates
A(15) = uint8(hex2dec('ff'));
A(16) = uint8(hex2dec('fe'));
A(17) = uint8(hex2dec('00'));
A(18) = uint8(hex2dec('00'));
A(19) = uint8(hex2dec('ff'));
A(20) = uint8(hex2dec('ea'));

%Accelerometers
A(21) = uint8(hex2dec('ff'));
A(22) = uint8(hex2dec('f8'));
A(23) = uint8(hex2dec('ff'));
A(24) = uint8(hex2dec('f7'));
A(25) = uint8(hex2dec('f3'));
A(26) = uint8(hex2dec('37'));

%Velocity
A(27) = uint8(hex2dec('00'));
A(28) = uint8(hex2dec('15'));
A(29) = uint8(hex2dec('fd'));
A(30) = uint8(hex2dec('a9'));
A(31) = uint8(hex2dec('fd'));
A(32) = uint8(hex2dec('4f'));

%GPS
A(33) = uint8(hex2dec('00'));
A(34) = uint8(hex2dec('00'));
A(35) = uint8(hex2dec('00'));
A(36) = uint8(hex2dec('00'));
A(37) = uint8(hex2dec('00'));
A(38) = uint8(hex2dec('00'));
A(39) = uint8(hex2dec('00'));
A(40) = uint8(hex2dec('00'));
A(41) = uint8(hex2dec('00'));
A(42) = uint8(hex2dec('00'));

%AHRS Temp
A(43) = uint8(hex2dec('2d'));
A(44) = uint8(hex2dec('19'));

%timeITOW
A(45) = uint8(hex2dec('00'));
A(46) = uint8(hex2dec('28'));
A(47) = uint8(hex2dec('8a'));
A(48) = uint8(hex2dec('3e'));

%BIT status Field
A(49) = uint8(hex2dec('03'));
A(50) = uint8(hex2dec('00'));

A(51) = uint8(hex2dec('00'));
A(51) = uint8(hex2dec('00'));
A(51) = uint8(hex2dec('00'));
A(51) = uint8(hex2dec('00'));
A(51) = uint8(hex2dec('00'));

end