guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
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The cost of the allowable transitions from the first layer to the second<br />
layer are shown below:<br />
004<br />
024<br />
040<br />
042<br />
044<br />
204<br />
224<br />
240<br />
2k2<br />
244<br />
400<br />
402<br />
404<br />
420<br />
422<br />
424<br />
440<br />
E<br />
\ FROM<br />
011<br />
To \<br />
3.162<br />
3.162<br />
3.162<br />
3.162<br />
4.242<br />
3.741<br />
3.741<br />
3.741<br />
3.741<br />
4.690<br />
5.009<br />
5.099<br />
5.099<br />
5.099<br />
5.830<br />
100<br />
3.000<br />
3.605<br />
5.000<br />
3.605<br />
4.123<br />
5.385<br />
5.000<br />
5.385<br />
6.403<br />
001<br />
3.000<br />
3.605<br />
5.000<br />
3.605<br />
4.123<br />
5.385<br />
5.000<br />
5.385<br />
6.403<br />
010<br />
3.000<br />
3.605<br />
5.000<br />
3.605<br />
4.123<br />
5.000<br />
5.385<br />
6.403<br />
101 110<br />
3.162<br />
3.741<br />
5.099<br />
3.162<br />
3.741<br />
5.099<br />
3.162<br />
3.162<br />
4.242<br />
3.741<br />
2-g<br />
5:099<br />
5.099<br />
5.830<br />
3.162<br />
3.714<br />
5.099<br />
3.162<br />
3.714<br />
5.099<br />
3.162<br />
3.741<br />
5.009<br />
3.162<br />
3.741<br />
5.099<br />
4.242<br />
4.609<br />
5.830<br />
111<br />
3.316<br />
3.316<br />
3.316<br />
3.316<br />
4%<br />
3:316<br />
3.316<br />
3.316<br />
';*;z<br />
3:316<br />
4';::<br />
3:316<br />
4.358<br />
4.358<br />
The blank areas represent transitions that are not allowed because of reasons<br />
previously stated. The transitions from the second layer to the terminal<br />
point are shown in the following table:<br />
19<br />
;*:;z<br />
.