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LM-30 UAV system Introduction

LM-30 UAV adopts frame or FS mode tube launch way, which is folded during storage and transportation, similar to cuboid. The unfolded state is a conventional layout, the fuselage is a blunt cuboid, and the middle and rear fuselage is modified to meet the folding requirements of the tail wing. The wing is a straight high-wing, which adopts single-axis rotation. The whole wing rotates 90°clockwise. The tail is an inverted V-tail, and the root is equipped with a rotating shaft, which can be folded forward on both sides of the fuselage. The power system of the whole aircraft is a pusher arrangement, and the propeller is driven by the motor. The propeller is a two-blade fixed-pitch folding propeller, which is folded backward at the tail of the fuselage. The booster is arranged right behind the motor at the tail of the fuselage.

Product characteristics

LM-30 UAV system Introduction

Figure1    Three views in the expanded state

LM-30 UAV system Introduction1

Figure2    Three views in folded state

Table1    UAV basic parameter

Item

Description

Parameter

1.

Aircraft size

Deployment status (length × wingspan × height):

1869 × 276 × 1900mm

Folded state (length × wingspan × height): 
2039 × 191 × 199mm

2.

Angle between unilateral

empennage and horizontal plane

35°

3.

Propeller diameter

23in

4.

Maximum launch weight

36kg

LM30 Specification

The main performance specification of LM-30 UAV are shown in the following table.

Figure1    Three views in the expanded state

Item Description Performance parameters
1 Payload weight 6~7kg
2 Maximum level flight 180km/h (EAS)
speed
3 Economic cruising speed 144km/h (EAS)
4 Maximum service climb 3m/s
rate
5 Practical ceiling 3000m
6 Minimum operating spiral 260m
radius
7 Voyage 200km
8 Endurance 80 min (altitude 1000m, speed 40m/s)
9 Mission radius 50km
10 Communication distance ≮50km (sight distance)
11 Image terminal guidance ≯1.5m
DJ accuracy
12 Satellite terminal guidance ≯10m
DJ accuracy
13 Visible light identifiable ≮4km (typical 3m × 3m × 6m vehicle)
locking distance
14 Infrared identifiable ≮1.2km (typical 3m × 3m × 6m vehicle)
locking distance
15 Laser ranging distance 50~3000m
16 FS wind resistance rating Level 6 (adjust the launching direction as required according
to the wind direction)
17 Level flight wind resistance ≮Level 7
rating
18 Waterproof grade Light rain (rainfall: ≯10mm/d)
19 System operating -25℃~60℃
temperature
20 Storage temperature -10℃~40℃
21 Mission capability Capable of performing tasks day and night
22 Resistance to dampness Normal operation at 40 ℃ and 95% RH
and heat
23 Resistance to mildew and It needs to be sealed and stored with film packaging, and its
salt spray use is not limited.
24 Anti-dust ability It shall be packaged and sealed with film for storage. It shall be used only in the weather of floating dust and blowing sand (horizontal visibility is above 1km). It is forbidden in the
weather of sandstorm.

Technical features of the product

a)It has the ability of heavy load, long endurance, rapid mobile deployment, zero long launch, wide performance envelope and precise attack on targets, and is suitable for various mission scenarios.

b)It has a variety of configurations of coordinate strike, reconnaissance and reconnaissance, and can quickly change the mission load according to customer needs.

c)Pure electric power system, tail rocket booster launch, with wing, tail folding and unfolding two modes of launch capability, friendly man- machine interface of ground station, high product maturity;

d)Adopt mature material machine technology, low cost, high performance, lightweight composite material structure design; The modular design is adopted, the structural design of the machine body is compact, and the comprehensive efficiency is high;

e)It is suitable for various complex environments such as damp heat, mildew, salt fog, sand and dust, etc. It has strong anti-wind ability for launching and flying, and can launch at an altitude of less than 3000 m.

f)High reliability, simple and convenient maintenance and test, andconvenient use and operation;

g)It has excellent performance, high cost-effectiveness ratio, and has the ability of swarm networking and saturation attack.

Product composition

LM-30 UAV system includes flight platform, command and control system, launching system and integrated support system. The flight system comprises a LM30 platform, an airborne datalink end and a gimbal camera.etc, the command and control system include a ground control station and a ground datalink; the launching system include a launcher device, a launching ignition system and a booster; The integrated support system includes packaging equipment and operation and maintenance equipment.

LM-30 UAV system Introduction2

Figure3 UAV system composition architecture

Energy Power System

1. Battery

The UAV is equipped with two rechargeable lithium-ion batteries as the energy source of the whole aircraft.

Table3    Parameters of lithium ion battery

Item

Description

Specification

1

Type of battery

14s lithium ion battery

2

Nominal capacity

36Ah

3

Charge and discharge cut-off voltage

35V~58.8V

4

Storage voltage

49.7V~53.2V

5

Weight

5.85kg

6

size

215mm×152mm×88mm

7

Output connector

AS120-F

8

Rechargeable temperature

-10℃~50℃

9

Operating ambient temperature

-20℃~55℃

10

Storage temperature

-20℃~35℃

11

Charging current

28A

2. Power system

The UAV power system consists of a motor with a maximum power of 7.5KW, an electric regulator with a maximum continuous working current of 120 A (good heat dissipation) and a two-blade propeller with a size of 23 inches. The performance parameters of the power system are shown in the table below.

Table4    Parameters of power system

Category Description Parameter
Propeller Propeller diameter 23in
Use the altitude 0-5000m
Material Carbon fiber composite
Electric machinery Size φ90mm×80.8mm
Weight 1115g
Power 10S-14S
Maximum power 7500W
Electric Tune Size 116mm×56mm×31.5mm
Weight 405g
Power 6S-14S
Current specification 200A

Electrical system

The power distribution system is composed of relay box, distribution box and cable assembly to complete the functions of UAV power access, secondary power conversion and power transmission. The relay box has the functions of power supply access, pre-charging and power-on, power-on self- locking and power-off. The distribution box has the function of secondary power supply conversion. The cable transmits the electric energy to each electrical equipment, as shown in the following figure.

The belly has a pull-out breakaway connector with the following functions:
a. Charge and discharge the battery on the machine;
b. Ground power access;
c. Maintenance interface of flight control computer (network port and mode switching interface);
d. Upper and lower electrical interfaces of UAV;
e. Rocket launch interlock interface.

LM-30 UAV system Introduction3

Figure4    Power distribution system diagram

Airborne data link

Airborne datalink is a bidirectional data link for UAV applications, which can transmit video data and measurement and control data at the same time. The airborne datalink uses a single antenna time-sharing multiplexing mode, which greatly reduces the total weight of the equipment, has simple connection, is convenient to install and integrate, and can be quickly deployed for work; Intelligent design is adopted to adjust the working frequency point, bandwidth and output power on site.

Table5 Airborne datalink parameter

Item

Description

Parameter

1

size

Airborne data terminal: 98.99x63.1x22.2mm

2

Weight

Airborne data terminal: 180g ± 5g

3

Operating temperature

-20 ~ 65℃

4

Storage temperature

-40 ~ 85℃

5

Operating voltage

Airborne data terminal: DC 9 ~ 32 V

6

RF power

2W(33dBm±1dBm)

7

RF bandwidth

15MHz

8

Power  consumption  of

the whole machine

Airborne data terminal: 30W

9

Operating frequency

band

1432MHz

10

Effective code rate

Uplink: 200kbps,

Downlink: 8Mbps, 4Mbps, 2Mbps, 250kbps (dynamically configurable)

11

Receive sensitivity

-99dBm@15MHz

12

Airborne antenna gain

Greater than 1 dBi

13

Ground  Omnidirectional

Antenna Gain

Greater than 1 dBi

14

Ground Directional

Antenna Gain

Greater than 15 dBi

15

Doppler shift

Up to 300Km/H relative motion speed

16

End-to-end delay

Video delay: ≯ 200ms (excluding video acquisition delay)

Data delay: ≯ 40ms

LM-30 UAV system Introduction4

Figure5 Airborne Datalink

Gimbal camera

The gimbal camera adopts a two-axis stabilized platform, installs a conductive slip ring to achieve 360 ° continuous rotation, and is equipped with a 30x high-definition visible light camera, a long-wave uncooled infrared imaging component, and a laser rangefinder. It is mainly used for ground imaging detection, identification, tracking, ranging and positioning, and meets the needs of aerial mapping, monitoring, survey, etc. Its important functional performance indicators are as follows.

A.Visible zoom camera
i.Working waveband: 0.4 μm ~ 0.9 μm;
ii.Resolution: 1920 × 1080;
iii.Focal length: 4.3mm ~ 129mm, optical 30x continuous zoom, 12x digital zoom;
iv.Optical zoom hFOV 63.7º ~ 2.3º;
v.Video output: Ethernet, 1080P, 30 Hz;

Target

Target Size (m)

Detection (Km)

Recognition(Km)

PEOPLE

0.5x1.8

6

2

VEHICLE

3x6

15

8

B.Uncooled LWIR
i.Operating band: 8 μm ~ 14 μm;
ii.Detector pixel number: 640 × 512;
iii.Pixel size: 12 um;
iv.NETD:50mk;
v.Focal length: 35mm/F1.0;
vi.Field angle: 12.5º × 10º;
vii.Video output: Ethernet, 1080P, 30 Hz.

Target

Target Size (m)

Detection (Km)

Recognition (Km)

PEOPLE

0.5x1.8

1

0.25

VEHICLE

3x6

6

1.5

C.Laser Rangefinder
i.Working wavelength: 1535nm;
ii.Ranging accuracy: ± 1 m;
iii.Ranging frequency: 5Hz;
iv.Laser ranging distance: 50-3000m

D.Servo System
i.Swing range
Azimuth axis: n × 360 ° continuous rotation
Pitch axis: -110 ° ~ + 10 ° (horizontal direction is 0 °, upward is positive)
ii.Angle measurement accuracy: ≤ 2mrad;
iii.Stabilization accuracy: ≤ 100µrad (1σ) (2 °/1Hz, 1 °/2Hz swing);
iv.Maximum angular velocity: ≥ 50 °/s;
v.Maximum angular acceleration: ≥ 90 °/s 2 .

E.Tracking Functions
i.Pixel deviation update rate: 50hz;
ii.Tracking speed: 30 pixels/frame;
iii.Minimum target contrast: 8%;
iv.Minimum target imaging size: 4 × 3 pixels;
v.In the case of rolling, rapid reduction or enlargement of target imaging, it has the ability of tracking without slippage and loss.
It has the ability to automatically recapture the target after the short-term occlusion of clouds and ground scenes is eliminated.

LM-30 UAV system Introduction5LM-30 UAV system Introduction6

Ground Control Station

The UAV system can be easily controlled from a portable computer, such as a laptop. In addition, the user can select the command module to improve the working conditions of the command and system operators. For the command module, the ground data link and power supply unit can also be integrated to make the system more convenient to use.

lm-30-uav-system-introduction7Figure7 Portable Ground Control Station

Ground Datalink

The ground datalink adopts a light PTZ, and the ground processing equipment is integrated inside the turntable, which is a completely integrated design. Appearance and dimensions of the ground datalink are shown in the figure below:

Table6 Ground Datalink Parameters

Item Description Parameter
1 Size Ground data terminal: 675x386.6 x156.9 mm
2 Weight Ground data terminal: 9500 G ± 100 G
3 Power consumption of Ground data terminal: 20W (rotary table
the whole machine stationary), 40W (rotary table rotating)
4 Operating voltage Ground data terminal: DC 24V
5 Rotation speed Level 0.01 ° ~ 30 °/s; Pitch 0.01 ° ~ 12 °/s
(continuously variable speed)
6 Rotation angle Horizontal: 0 ~ 360 ° continuous rotation
Elevation: + 20 ° ~ -20 °
7 Angular resolution 0.5°
8 Power consumption of ≤30W
the whole machine
9 Quiescent power 5W
consumption
10 Operating -20    ~ + 55   , 90% ± 3%, non-
temperature condensing
11 Storage temperature -40℃~+65
LM-30 UAV system Introduction8

Figure8  Ground Datalink

Launcher

Dimension of single launch tube: 300mm × 250mm × 2600mm, material: glass fiber + partial metal structure, weight: about 50kg

LM-30 UAV system Introduction9LM-30 UAV system Introduction11

Figure9    Schematic diagram of vehicle-mounted launcher

Launch ignition system

The launch ignition control system consists of an adapter box, a control box, a 6S rocket ignition battery and a cable, which can realize the functions of UAV power on and off, on-board battery charging, launch interlock control, rocket ignition, etc.

QQ20250928-153412

Figure10    Electrical Block Diagram of Launch Ignition System

a) The adapter box and the control box are used to realize the functions of aircraft power on and off and rocket ignition control, wherein the adapter box is fixed on the launcher, and the control box is placed in the ignition safety area:

1) The arrangement of the panel of the switching box is described as follows:
A. Voltage display: used to display the aircraft battery voltage;
B. Safety: used to protect the ignition battery;
C. Charging and discharging interface: used to maintain the aircraft battery without disassembling the aircraft battery;
D. Ignition battery interface: used to connect the ignition battery and provide power for the adapter box and control box;
E. X1 connector: a 16-core waterproof connector is used to connect the aircraft through the adapter cable. The red dot on the plug of the adapter cable is aligned with the red dot on the X1 connector for plugging. The connection is completed after the locking sound is heard.
F. X2 connector: 2-core waterproof connector is used to connect the booster rocket;
G. X3 connector: a 12-core waterproof connector is used to connect the control box through the adapter cable.

LM-30 UAV system Introduction12

Figure11    Physical drawing of the adapter box

2)The layout of the control box panel is described as follows:
A. Power-on switch: a self-reset switch is used to power on the aircraft, and it needs to be pressed for 3s.
B. Power-off switch: a self-reset switch is used to power off the aircraft, and it needs to be pressed for 3s.
C. Ignition switch: It is a self-reset knob switch. When the arrow isupward, it is closed. It can be opened by rotating clockwise to ignite the rocket booster. When igniting, it is held for 1 second after rotating clockwise.
D. Power-on indicator: used to indicate the power-on condition of the aircraft;
E. Disarming indicator: used to indicate the unlocking condition of the ground station software;
F. Ignition indicator: It is used to indicate the energization of pin 2 of the X2 connector of the junction box. When the ignition indicator is on, the X2 connector is energized and the rocket booster is ignited.

LM-30 UAV system Introduction13

Figure12    Physical drawing of control box

b)The ignition battery is used to provide energy for the control drive and booster rocket in the adapter box. The parameters of the battery are described in the following table.

Table7    Main parameters of single lithium polymer battery

Access mode

6S1P

Nominal capacity

4000mAh @ 2C Discharge

Nominal voltage

22.8V(Cell 3.80V)

Size

MAX(T*W*L):170×50×38mm

Weight

620g

Booster

Rocket Booster: Provide the overall thrust of the UAV during launch to ensure that the aircraft can reach the initial flight speed and altitude. The booster is installed at the tail of the aircraft and is detached after operation. The rocket booster and its installation are shown in the figure below.

Table8    Booster parameters

Description

Parameter indicators

Weight/kg

3.2

Diameter/mm

82

Length/mm

335

Total stroke/N • s

2600

Average thrust/N

1857

Working time/s

1.4

LM-30 UAV system Introduction14

Figure13 Schematic diagram of the rocket booster