lab03 - Electronic Navigation Systems Lab 3 Part 1 Show...

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Unformatted text preview: Electronic Navigation Systems Lab 3 Part 1 Show that for a stationary inertial navigation system, the -angle error equations given by r n v n = - n e/n I G- 2 n i/e + n e/n ( f n )- n i/e + n e/n r n v n + f n + g n reduce to r N r E r D v N v E v D N E D = 1 1 1- g R- 2 i/e s g- g R 2 i/e s 2 i/e c - g 2 g R- 2 i/e c - i/e s i/e s i/e c - i/e c r N r E r D v N v E v D N E D + f N + g N f E + g E f D + g D N E D ....
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lab03 - Electronic Navigation Systems Lab 3 Part 1 Show...

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