TL32 Datasheet, PDF (28/31 Pages) List of Unclassifed Manufacturers – Real Time System Testing MIT 16.070 Lecture 32

Section 4 - Requirements Traceability (continued)
Rqmt #
12
13
14
15
16
17
17
18
Description
The simulator will have three types of output. It will:
1. send information to the controller specifying altitude, velocity, and whether
there is fuel remaining;
The simulator will have three types of output. It will:
2. call a graphics package (provided) that will display a representation of the
lander as it descends. The simulator must determine the condition of the vehicle
using one of four conditions defined in the Graphics Package Interface section
(see "vehicle-condition" variable);
The simulator will have three types of output. It will:
3. write altitude, velocity, thrust and fuel remaining information to a telemetry
file using the same format as the simulation in PS8 (plus a fuel remaining
column), and write an error message to the telemetry file if the graphics package
returns an error condition.
The simulation will end when the vehicle reaches 0 meters of altitude or goes
above its initial altitude.
Simulation code will interface to the provided graphics package
The serial interface should be used to continually send data back and forth
between the simulation and the controller.
Data sent from the simulation to the controller shall correspond to the provided
interface specification
Data sent from the controller to the simulation shall correspond to the provided
interface specification
Method
Test
Test
Test
Test
(see rqmt 3)
Test
Demo
Test
Test
Test
Test (if applicable)
hperry
5/4/01