This document summarizes an amateur unmanned aerial vehicle (UAV) project being undertaken by Shailendra Singh and Priya Ranjan. It describes the specifications of their UAV, which includes an At-mega128 microcontroller, GPS, gyroscope, and accelerometer sensors. It outlines the phases of the project, including initial remote control, then semi-autonomous and fully autonomous flight. Diagrams show the basic aircraft layout and sensors. The document also discusses UAV classification and applications, as well as future prospects like swarm UAVs and advanced vehicle management systems.

1. Shailendra Singh#1, Priya Ranjan*2
#Electronics and Communication engineering,
Team leader, Team “SURYAAN”, Kanpur, UP, India
1srj0408@gmail.com
*Human Development Foundation
Bhuvneswar, Orissa, India
2pranjan@gmail.com
Towards a new low cost, simple
implementation using embedded
system wireless
Networking for UAVs
IEEE
ANTS
2011

2. UAV(UNMANNED AERIAL
VEHCILE)

3. A Unmanned Aerial Vehicle (UAV) is an
uncrewed aircraft .
Or
A UAV can be defined as an
aircraft flying in auto pilot mode or
manual mode with various
operation to be performed feeded
inside it or to be controlled by
GCS.
Definition

4. UAV classification
●
Handheld 2,000 ft (600 m) altitude, about 2 km range
●
Close 5,000 ft (1,500 m) altitude, up to 10 km range
●
NATO type 10,000 ft (3,000 m) altitude, up to 50 km range
●
Tactical 18,000 ft (5,500 m) altitude, about 160 km range
●
MALE (medium altitude, long endurance) up to 30,000 ft
(9,000 m) and range over 200 km
●
HALE (high altitude, long endurance) over 30,000 ft and
indefinite range
●
HYPERSONIC high-speed, supersonic (Mach 1-5) or
hypersonic (Mach 5+) 50,000 ft (15,200 m) or suborbital
altitude, range over 200km
●
ORBITAL low earth orbit (Mach 25+)
●
CIS Lunar Earth-Moon transfer

5. 1) Remote sensing
2) Transport
3) Scientific research
4) Armed attacks
UAV FUNCTIONS

6. AMATEUR UAV:-
AMATEUR because-
1)It will be not be made on industrial scale and will be a
research cum project cum hobby.
2)It is not powered by a jet or a reciprocating engine.
3)Low speed.
4)Range of operation is less.
5)Cannot carry more weight.
6)Camera resolution and accuracy is less.
OUR PROJECT:-

7. PROJECT SPECIFICATIONS
● An Aero-model with a auto-pilot kit that will be made by me. Presently
working on its PCB layout. Kit will include:-
● 1) At-mega128
● 2) GPS (GPS receiver with antenna-5V TTL)
● 3) Gyroscope (single axis ±300 °/Second Analog Yaw Gyroscope
module)
● 4) MMA7361L ±1.5g, ±6g Three axis Low-G Accelerometer Module.
● 5) pitot tube (KIT MPXV5004DP)(optional)
● 6) Camera and zigbee-pro.
● 7)Magnetic compass HMC 6352
● 8) Ground control station(HK GCS)

8. Basic layout of aero-model
●
A=auto-pilot control board
●
B=battery
●
D=datalink radio modem and antenna
●
G=GPS receiver
●
I=accelerometer module
●
M=motor and
controller
●
RC receiver and
antenna
●
S=servo
●
P=payload
(camera and
video Trx)

9. PHASES OF PROJECT
●
1st PHASE:- Remote controlled spy.
●
2nd PHASE:-Semi auto-pilot.
●
3rd PHASE:-Fully auto-pilot.

10. Aeromodelling

11. Sensors

12. EMBEDDED SYSTEM

13. GENERAL LAYOUT

14. Algorithm
Program where
Destination GPS
coordinates are
placed
Program where
distance and elivation
between 2
coordinates is find out
using HAVERSINE
FORMULA
Program where
Elivation of the
aeromodel is find out
using
GYROSCOPE AND ACCE
LEROMETER
Programm to take the
OUTPUT of GPS in
GGA AND RMC format
.
Programm to generate
the PWM for the
servo to control the
aircraft surface.
Program for PID
feedback loop. which
will tell us that the
required elivation angle
has been covered by
the Aeromodel or not.
Central program
which will take I/P
from all other
programs and direct
the aeromodel to
move through
different coordinates
as directed

15. GCS(Ground control
software)

16. GCS(Ground control
software in USA)

17. GPS WITH X-CTU

18. FUTURE PROSPECTS
Swarm UAV’s

19. ADVANCE VEHICLE
MAMAGEMENT SYSTEM

20. Some Work in LAB:-

21. CONTINUED…..

22. MQ1-B Predator

23. Indian UAV’s by DRDO
•DRDO Lakshya
•DRDO Nishant
•DRDO Rustom
•DRDO Kapothaka
•DRDO Fluffy
•DRDO Ulka
•DRDO AURA

24. Indian UAV’s by DRDO
•DRDO LAKSHYA
General characteristics
Crew: None
Length: 2385 mm ()
Wingspan: 3m ()
Height: (500-5000 m)
Wing area: 2.27 m2 ()
Airfoil: NACA64A008
Max takeoff weight: 705 kg (1554 lb)
Powerplant: 1 × HAL PTAE-7 turbojet
Maximum speed: Mach 0.7
Range: 150 km (93.2 mi)
Service ceiling: 9000 m (5000 m with towed sub-target)
Rate of climb: 25 m/s ()

25. DRDO NISHANT
General characteristics
•Crew: None
•Length: 4.63 m (15.2 ft)
•Wingspan: 6.57 m (21.6 ft)
•Height: ()
•Empty weight: 380 kg (840 lb)
•Useful load: 45 kg (99 lb)
•Powerplant: 1× RE-2-21-P or RE-4-37-P, ()
Performance
•Maximum speed: 185 km/h
•Cruise speed: 125 km/h to 150 km/h
•Range: 160 km (100 mi)
•Service ceiling: 3,600 m (up to 11,800 ft)

26. DRDO RUSTAM
General characteristics
•Crew: none
•Length: ()
•Wingspan: 20 m (65.616 ft)
•Height: ()
•Empty weight: 1,800 kg (3968.32 lbs)
•Powerplant: 1× , ()
Performance
•Maximum speed: 225 km/h (139.81 mph)
•Range: 350 km ()
•Service ceiling: 35,000 ft (10,668 m)