lampiran a gambar sistem - repository.maranatha.edu file// func7=in func6=in func5=in func4=in...

LAMPIRAN A

GAMBAR SISTEM

SISTEM OBJEK TAMPAK DALAM

SISTEM OBJEK TAMPAK LUAR

SISTEM PENERIMA

LAMPIRAN B

PROGRAM AVR ATMEGA 128

/*****************************************************

Chip type : ATmega128L

Program type : Application

Clock frequency : 11.059200 MHz

Memory model : Small

External SRAM size : 0

Data Stack size : 1024

*****************************************************/

#include <mega128.h>

#include <delay.h>

#include <math.h>

#include <stdlib.h>

unsigned char g[16]; //tampungan data

// Alphanumeric LCD Module functions

// I2C Bus functions

#asm

.equ __lcd_port=0x1B ;PORTA

.equ __i2c_port=0x15 ;PORTC

.equ __sda_bit=0

.equ __scl_bit=1

#endasm

#include <lcd.h>

#include <i2c.h>

#define RXB8 1

#define TXB8 0

#define UPE 2

#define OVR 3

#define FE 4

#define UDRE 5

#define RXC 7

#define FRAMING_ERROR (1<<FE)

#define PARITY_ERROR (1<<UPE)

#define DATA_OVERRUN (1<<OVR)

#define DATA_REGISTER_EMPTY (1<<UDRE)

#define RX_COMPLETE (1<<RXC)

// Get a character from the USART1 Receiver

#pragma used+

char getchar1(void)

{

char status,data;

while (1)

{

while (((status=UCSR1A) & RX_COMPLETE)==0);

data=UDR1;

if ((status & (FRAMING_ERROR | PARITY_ERROR |

DATA_OVERRUN))==0)

return data;

};

}

#pragma used-

// Write a character to the USART1 Transmitter

#pragma used+

void putchar1(char c)

{

while ((UCSR1A & DATA_REGISTER_EMPTY)==0);

UDR1=c;

}

#pragma used-

// Standard Input/Output functions

#include <stdio.h>

// Declare your global variables here

void main(void)

{

unsigned char string[10];

unsigned char buf,x;

float h_bar;

unsigned int temp,pressure; // bilangan bulat 0-6355

unsigned char temp1,temp2;

// Input/Output Ports initialization

// Port A initialization

// Func7=In Func6=In Func5=In Func4=In Func3=In Func2=In Func1=In

Func0=In

// State7=T State6=T State5=T State4=T State3=T State2=T State1=T State0=T

PORTA=0x00;

DDRA=0x00;

// Port B initialization


Func0=In


PORTB=0x00;

DDRB=0x00;

// Port C initialization


Func0=In


PORTC=0x00;

DDRC=0x00;

// Port D initialization


Func0=In


PORTD=0x00;

DDRD=0x00;

// Port E initialization


Func0=In


PORTE=0x00;

DDRE=0x00;

// Port F initialization


Func0=In


PORTF=0x00;

DDRF=0x00;

// Port G initialization

// Func4=In Func3=In Func2=In Func1=In Func0=In

// State4=T State3=T State2=T State1=T State0=T

PORTG=0x00;

DDRG=0x00;

// Timer/Counter 0 initialization

// Clock source: System Clock

// Clock value: Timer 0 Stopped

// Mode: Normal top=FFh

// OC0 output: Disconnected

ASSR=0x00;

TCCR0=0x00;

TCNT0=0x00;

OCR0=0x00;




// Mode: Normal top=FFFFh

// OC1A output: Discon.

// OC1B output: Discon.

// OC1C output: Discon.

// Noise Canceler: Off

// Input Capture on Falling Edge

// Timer 1 Overflow Interrupt: Off

// Input Capture Interrupt: Off

// Compare A Match Interrupt: Off

// Compare B Match Interrupt: Off

// Compare C Match Interrupt: Off

TCCR1A=0x00;

TCCR1B=0x00;

TCNT1H=0x00;

TCNT1L=0x00;

ICR1H=0x00;

ICR1L=0x00;

OCR1AH=0x00;

OCR1AL=0x00;

OCR1BH=0x00;

OCR1BL=0x00;

OCR1CH=0x00;

OCR1CL=0x00;




// Mode: Normal top=FFh

// OC2 output: Disconnected

TCCR2=0x00;

TCNT2=0x00;

OCR2=0x00;




// Mode: Normal top=FFFFh

// Noise Canceler: Off

// Input Capture on Falling Edge

// OC3A output: Discon.

// OC3B output: Discon.

// OC3C output: Discon.

// Timer 3 Overflow Interrupt: Off

// Input Capture Interrupt: Off

// Compare A Match Interrupt: Off

// Compare B Match Interrupt: Off

// Compare C Match Interrupt: Off

TCCR3A=0x00;

TCCR3B=0x00;

TCNT3H=0x00;

TCNT3L=0x00;

ICR3H=0x00;

ICR3L=0x00;

OCR3AH=0x00;

OCR3AL=0x00;

OCR3BH=0x00;

OCR3BL=0x00;

OCR3CH=0x00;

OCR3CL=0x00;

// External Interrupt(s) initialization

// INT0: Off

// INT1: Off

// INT2: Off

// INT3: Off

// INT4: Off

// INT5: Off

// INT6: Off

// INT7: Off

EICRA=0x00;

EICRB=0x00;

EIMSK=0x00;

// Timer(s)/Counter(s) Interrupt(s) initialization

TIMSK=0x00;

ETIMSK=0x00;

// USART0 initialization

// Communication Parameters: 8 Data, 1 Stop, No Parity

// USART0 Receiver: On

// USART0 Transmitter: On

// USART0 Mode: Asynchronous

// USART0 Baud Rate: 9600

UCSR0A=0x00;

UCSR0B=0x18;

UCSR0C=0x06;

UBRR0H=0x00;

UBRR0L=0x47;

// USART1 initialization

// Communication Parameters: 8 Data, 1 Stop, No Parity

// USART1 Receiver: On

// USART1 Transmitter: On

// USART1 Mode: Asynchronous

// USART1 Baud Rate: 4800

UCSR1A=0x00;

UCSR1B=0x18;

UCSR1C=0x06;

UBRR1H=0x00;

UBRR1L=0x8F;

// Analog Comparator initialization

// Analog Comparator: Off

// Analog Comparator Input Capture by Timer/Counter 1: Off

ACSR=0x80;

SFIOR=0x00;

// LCD module initialization

lcd_init(16);

// I2C Bus initialization

i2c_init();

while (1) // looping

{

buf=0;

while (buf!='$') buf=getchar1();

getchar1();

getchar1();

getchar1();

buf=getchar1();

if (buf=='G')

{

for (x=0;x<9;x++)

{

buf=0;

while (buf!=',') buf=getchar1();

}

buf=0;

x=0;

while (buf!=',')

{

buf=getchar1();

string[x]=buf;

x++;

}

x--;

string[x]=0;

buf=0;

while (buf!=0x0A) buf=getchar1();

printf("GPS:");

printf("%6s",string);

printf(" m ");

sprintf(g,"GPS= %s M ",string); //data gps

lcd_gotoxy(0,0);

lcd_puts(g);

i2c_start(); // Start Condition

i2c_write(0xE0); // Tulis ke modul DT-SENSE

i2c_write(0x00); // Perintah baca data tekanan

i2c_stop(); // Stop Condition

delay_ms(15); // delay 15 ms

i2c_start(); // Start Condition

i2c_write(0xE1); // Baca ke modul DT-SENSE

temp1 = i2c_read(1);

temp2 = i2c_read(0);

i2c_stop(); // Stop Condition

pressure = (unsigned int)temp1*256 + temp2;

h_bar=(float)pressure/10;

h_bar=h_bar/1013.25;

h_bar=log10(h_bar);

h_bar=h_bar/5.2558797;

h_bar=pow(10,h_bar)-1;

h_bar=h_bar*1000000/-6.87559;

h_bar=h_bar*0.3048;

ftoa(h_bar,2,string);

printf("Pressure: ");

temp=pressure/10;

printf("%u",temp);

putchar('.');

temp=pressure%10;

printf("%u",temp);

printf(" hpa ");

printf("H_Bar:");

printf("%7s",string);

printf(" m\n\r ");

sprintf(g,"H_Bar=%s M ",string); //data ketinggian dari tekanan

lcd_gotoxy(0,1);

lcd_puts(g);

}

};

}

LAMPIRAN C

CODE VISUAL BASIC

Public Dat_payload As Integer

Public sercount As Integer

Public buff_ser As Byte

Private Sub Command10_Click()

RichTextBox1.SaveFile Text13.Text

MsgBox ("DATA TERSIMPAN")

End Sub


If MSComm1.PortOpen = False Then MSComm1.PortOpen = True

End Sub


If MSComm1.PortOpen = True Then MSComm1.PortOpen = False

End Sub


End

End Sub


MSComm1.CommPort = Text9.Text

MSComm1.Settings = Text12.Text & ",n,8,1"

MSComm1.Handshaking = comNone

End Sub

Private Sub MSComm1_OnComm()

buff_ser = MSComm1.Input

Text7.Text = buff_ser

End Sub

Private Sub Text10_Change()

Dim a As String

Dim b As String

Dim c As String

a = Mid(Text10.Text, 5, 6) ' indikasi GPS

Text1(1).Text = a

b = Mid(Text10.Text, 23, 6) ' indikasi PREASURE

Text1(2).Text = b

c = Mid(Text10.Text, 40, 6) ' indikasi H_BAR

Text1(3).Text = c

End Sub

Private Sub Timer2_Timer()

If MSComm1.PortOpen = True Then

Text10.Text = MSComm1.Input

RichTextBox1.Text = Time & " ; " & Text10.Text & " ; " & Chr$(13) &

RichTextBox1.Text

End If

End Sub

LAMPIRAN D

DATA SHEET

Data Sheet GPS

ADS-GM1 GPS Receiver

The ADS-GM1 is a high-sensitivity GPS receiver based on the SiRFstar III

chipset. It has a 2-meter long cable terminated in a female DB9 connector that

allows direct connection to an OpenTracker+, Tracker2, or any other device that

provides regulated 5-volt power on pin 4.

SiRFstar III high-sensitivity chipset

Waterproof housing (IPX7 rating)

Built-in low noise, high gain antenna

Magnetic base

LED clearly indicates positioning status

No configuration required

20 channel all-in-view tracking

Sensitivity: -159 dBm typical

Accuracy: < 10 meters 2D RMS, < 7 meters WAAS corrected, time to 1

microsecond

Datum: WGS84

Acquisition Rate: 1 sec hot start, 42 sec cold start

Dynamic Limits: < 18,000 meters, < 1000 knots, < 4G acceleration

Power Supply: 5 VDC +/- 5%, 80 mA max, 55 mA typical

Interface: NMEA-0183 at 4800 baud, optional SiRF binary

NMEA Messages: GGA, GSA, GSV, RMC, and optionally VTG, GLL, and ZDA

Weight: 85 grams

LED flashes red to indicate valid GPS fix. Made in Taiwan.

Pin Wire Function

2 Red RS-232 data out (+/- 6v)

3 Brown RS-232 data in

4 Green Power in

5 Blue Ground

- Yellow TTL data out (0-3v)

- Black TTL data in

Data Sheet Sensor Tekanan

Data Sheet ATMega 128

Konversi Ketinggian Terhadap Tekanan

Altitude Units to Pressure Units Conversion Table

Convert from an altitude in feet or metres above sea

level to a pressure reading in millibar (mbar, mb or

mbr), hectopascals (hPa), pounds per square inch (psi), millimetres of mercury at zero degrees celsius

(mmHg @ 0 deg C) or inches of mercury at zero

degrees celsius ( inHg @ 0 deg C).

The height relative to sea level conversions are derived

using the US Standard Atmosphere 1976 barometric

formula for geopotential altitude with the following physical constants and multi-valued (*) constants for sea level up

to a height of 36,089 ft (11,000m)

1. *Standard atmospheric pressure of 1013.25 mb

absolute at sea level

2. *Standard temperature of 288.15 K (15°C) 3. *Standard thermal gradient or lapse rate of -0.0065

K/m increase in altitude

4. Standard acceleration due to gravity of 9.80665 m/s2

5. Gas constant for air of 8.31432 J/Kmol K

6. Molar mass of air of 0.0289644 kg/mole

Please note that the calculated altitude values are not

absolutely precise conversions and should not be treated as such.

Altitude to Pressure Conversion Table

-5000 ft -1524.0 m is 1210.23 mb/hPa 17.553 psi 907.75 mmHg 35.738 inHg









http://www.sensorsone.co.uk/pressure-measurement-glossary/mbar-millibar-pressure-unit.html

http://www.sensorsone.co.uk/pressure-measurement-glossary/mbar-millibar-pressure-unit.html

http://www.sensorsone.co.uk/pressure-measurement-glossary/hpa-hectopascal-pressure-unit.html

http://www.sensorsone.co.uk/pressure-measurement-glossary/psi-pounds-per-square-inch-pressure-unit.html

http://www.sensorsone.co.uk/pressure-measurement-glossary/psi-pounds-per-square-inch-pressure-unit.html

http://www.sensorsone.co.uk/pressure-measurement-glossary/mmhg-millimetres-mercury-0-deg-c-pressure-unit.html

http://www.sensorsone.co.uk/pressure-measurement-glossary/mmhg-millimetres-mercury-0-deg-c-pressure-unit.html

http://www.sensorsone.co.uk/pressure-measurement-glossary/inhg-inch-of-mercury-0-deg-c-pressure-unit.html



http://en.wikipedia.org/wiki/U.S._Standard_Atmosphere

http://en.wikipedia.org/wiki/Barometric_formula

http://en.wikipedia.org/wiki/Barometric_formula






-50 ft 15.240 m is 1015.08 mb/hPa 14.723 psi 761.37 mmHg 29.975 inHg

0 ft 0 m is 1013.25 mb/hPa 14.696 psi 760.00 mmHg 29.921 inHg

50 ft 15.240 m is 1011.42 mb/hPa 14.669 psi 758.63 mmHg 29.867 inHg
























35000 ft 10668 m is 238.423 mb/hPa 3.4580 psi 178.83 mmHg 7.0406 inHg

Rumus Ketinggian Terhadap Tekanan

Z meters = ( 1 - ( P/ 1013.25 )^ 0.19 ) ) / 22.558 E-6

Altitude = (10^(log(P/P_0)/5.2558797)-1)/-6.8755856*10^-6.

Where P is the pressure at an unknown altitude, and P_0 is the pressure at sea

level (zero feet). P and P_0 can be expressed in any unit because they are

computed as a ratio.

lampiran a gambar sistem - repository.maranatha.edu file// func7=in func6=in func5=in func4=in...

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