ApolloModellierung und Simulation eines Raumschiffs

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Apollo Guidance Systems

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Modellerstellung

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Flugphasen

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DESIRED EQUILIBRIUM PATH I

/ J+’ DESIRED STABILIZATION, I / a I

VELOCITY VECTOR/ I /’\ EXISTING

EQUILIBRIUM PATH

REFERENCE COORDINATES VELOCITY VECTOR

IN VELOCITY VECTOR

-COMMANDED CHANGE IN STABILIZATION REFERENCE / /

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REFERENCE COORDINATES / N cn / 4 I DESIRED

I STAB1 L IZATION /

/ REFERENCE PATH

/ /

GE IN STABILIZATION REFERENCE PATH - __ - --” - --- “ G T A B I L I Z A T I O N REFERENCE PATH

MANEUVER IS THE PROCESS OF CHANGING THE STABILIZATION REFERENCE COORDINATES AND VECTOR VELOCITY SO THAT VEHICLE ORIENTATION AND VELOCITY LEAD TO MISSION SUCCESS

Fig. I- 12 Maneuver

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Simulink-Modell

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David A. Mindell

20. bis 24. Mai in Ulm12

Institut für eingebettete SystemeEchtzeitsysteme Universität UlmES

Prof. Dr.-Ing. Frank Slomkawww.uni-ulm.de/in/esys

Donnerstag, 18. April16 Uhr

O27/31213