1. A method for automatically generating documentation for a design, comprising:
embedding comments into at least two source files having distinct types, each source file defining an aspect of the design;
creating a configuration file including parameters associated with each type of source file; and
extracting the comments from each source file responsive to the parameters associated with each type of source file to create the documentation;
wherein extracting comments includes parsing each source file for keywords;
wherein parsing each source file for keywords comprises:
parsing each source file for a change log keyword;
parsing each source file for a title keyword;
parsing each source file for a section keyword; and
parsing each source file for a register keyword.
2. The method of claim 1 comprising creating a first source file using a source software different than that used to create remaining source files.
3. The method of claim 1 wherein creating a configuration file includes verifying a valid output file.
4. The method of claim 1 comprising:
extracting source file directory information from one of the parameters included in the configuration file; and
opening the source file directory.
5. The method of claim 1 comprising building a database with the comments extracted from each source file.
6. The method of claim 1 comprising parsing the comments extracted from each source file for object references.
7. The method of claim 1 comprising parsing the comments extracted from each source file for headings.
8. A method for automatically generating documentation for a design, comprising:
embedding comments into a plurality of source files defining the design;
creating a configuration file including parameters associated with each source file;
extracting the comments from each source file responsive to the parameters; and
building an output document from the comments extracted from each source file, the output document being any one of an IRS, ERS, HUG, EN, and VP document;
where building an output document includes:
building section pages;
creating a table of included registers; and
creating a change log page.
9. The method of claim 8 wherein building an output document includes automatically keeping track of document revisions.
10. The method of claim 8 wherein building an output document includes automatically tracking hyper links and comment character definitions.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. A method for controlling a deceleration profile of an aircraft, comprising:
receiving, with a processor, a signal indicative of a deceleration command;
receiving with the processor, signals indicative of a sensed velocity and a commanded heading rate;
determining, with the processor, a commanded velocity in response to the receiving of the deceleration command and the commanded heading rate;
determining, with the processor, an estimated deceleration command as a function of the commanded velocity; and
determining, with the processor, an actual deceleration command in response to the determining of the estimated deceleration command.
2. The method of claim 1, wherein the receiving of the deceleration command further comprises receiving longitudinal and lateral deceleration commands.
3. The method of claim 1, wherein the determining of the commanded velocity further comprises determining a commanded longitudinal velocity and a commanded lateral velocity.
4. The method of claim 3, further comprising determining a longitudinal velocity error signal indicative of a difference between the commanded longitudinal velocity and a sensed longitudinal velocity.
5. The method of claim 3, further comprising determining a lateral velocity error signal indicative of a difference between the commanded lateral velocity and a sensed lateral velocity.
6. The method of claim 1, further comprising determining a commanded acceleration in response to the receiving of the deceleration command.
7. The method of claim 6, further comprising determining a second error value indicative of a difference between the commanded acceleration and a sensed acceleration.
8. The method of claim 4, further comprising determining a longitudinal commanded gain ratio as a function of the longitudinal velocity error signal and a total velocity magnitude.
9. The method of claim 8, further comprising determining a lateral commanded gain ratio as a function of the lateral velocity error signal and a total velocity magnitude.
10. The method of claim 9, further comprising determining the estimated deceleration command as a function of the total velocity magnitude.
11. The method of claim 1, further comprising determining a Translational Rate Command response wherein controller deflection correlates to steady state velocity.
12. A system for controlling a deceleration profile of an aircraft, comprising a propeller comprising a plurality of blades, wherein the propeller is associated with a sensor;
a processor; and
memory having instructions stored thereon that, when executed by the processor, cause the system to:
receive a signal indicative of a deceleration command;
receive signals indicative of a sensed velocity and a commanded heading rate;
determine a commanded velocity in response to the receiving of the deceleration command and the commanded heading rate;
determine an estimated deceleration command as a function of the commanded velocity; and
determine an actual deceleration command in response to the determining of the estimated deceleration command.
13. The system of claim 12, wherein the processor is configured to receive longitudinal and lateral deceleration commands.
14. The system of claim 12, wherein the processor is configured to determine a commanded longitudinal velocity and a commanded lateral velocity.
15. The system of claim 14, wherein the processor is configured to determine a longitudinal velocity error signal indicative of a difference between the commanded longitudinal velocity and a sensed longitudinal velocity.
16. The system of claim 14, wherein the processor is configured to determine a lateral velocity error signal indicative of a difference between the commanded lateral velocity and a sensed lateral velocity.
17. The system of claim 12, wherein the processor is configured to determine a commanded acceleration in response to the receiving of the deceleration command.
18. The system of claim 17, wherein the processor is configured to determine a second error value indicative of a difference between the commanded acceleration and a sensed acceleration.
19. The system of claim 15, wherein the processor is configured to determine a longitudinal commanded gain ratio as a function of the longitudinal velocity error signal and a total velocity magnitude.
20. The system of claim 16, wherein the processor is configured to determine a lateral commanded gain ratio as a function of the lateral velocity error signal and a total velocity magnitude.