WHAT YOU GET
Technical Content Breakdown
Every parameter explained. Understand exactly what data you receive at each tier before you buy.
MODULE 01
Wing Loading Analysis
ALPHA · TIER 1+
- W/S (kg/m²)
- span loading
- stall speed
- manoeuvre envelope
Wing loading W/S determines stall speed, cruise efficiency, and gust response. Both platforms compared. Includes V-n diagram and operating envelope boundary.
MODULE 02
Lift Curve (CL vs α)
ALPHA · TIER 1+
- CL max
- α stall
- dCL/dα
- zero-lift α
Tabulated and plotted lift curve for the primary aerofoil section. Includes clean and flaps-extended configurations for both UAV platforms.
MODULE 03
Drag Estimate
ALPHA · TIER 1+
- CD0
- induced drag
- interference
- CD total
Component drag build-up using flat-plate skin friction and form factors. Parasite drag breakdown by fuselage, wing, tail, nacelle, and undercarriage.
MODULE 04
Power Required vs Speed
ALPHA · TIER 1+
- P_req (kW)
- V_min power
- V_max range
- endurance speed
Power curves plotted from stall to VNE. Minimum power speed, best-range speed, and best-endurance speed annotated. Covers sea level and cruise altitude.
MODULE 05
Aerospace Research Paper
BETA · TIER 2+
- abstract
- methodology
- results
- references
Structured research paper documenting the UAV design rationale, comparative analysis between turboprop and pusher configurations, and key performance projections. IEEE-style formatting.
MODULE 06
Flight-Validated Design Basis
BETA · TIER 2+
- design point
- payload fractions
- fuel fractions
- Breguet range
Mission segment fuel fractions using Breguet range equation. Payload-range trade study. Weight build-up with validated fractions benchmarked against comparable MALE-class platforms.
MODULE 07
Prototype Specification
BETA · TIER 2+
- materials
- dimensions
- systems list
- weight budget
Complete prototype specification sheet for both UAV-LRS-2000 and UAV-PSH-001 including airframe materials, structural sections, systems list, and full weight budget table.
MODULE 08
Lift Coefficient Dataset
DELTA · TIER 3+
- CL_cruise
- CL_max
- CL_to
- CL_land
Full lift coefficient table across angle of attack from −4° to stall. Cruise CL, take-off CL, landing CL and their corresponding Mach/speed conditions. High-lift device effect.
MODULE 09
Drag Polar
DELTA · TIER 3+
- CD vs CL²
- Oswald factor
- L/D max
- polar intercept
Full drag polar CD = CD0 + CL²/(π·AR·e) plotted with Oswald efficiency factor. L/D max and the corresponding flight condition. Flaps-up and flaps-down polars.
MODULE 10
Reynolds Number Analysis
DELTA · TIER 3+
- Re_cruise
- Re_stall
- aerofoil regime
- transition point
Chord Reynolds numbers at cruise, stall, and climb conditions. Laminar-turbulent transition analysis. Aerofoil selection validation — confirms low-Re regime suitability for MALE-class operation.
MODULE 11
Propulsive Efficiency
DELTA · TIER 3+
- η_prop
- η_thermal
- η_overall
- thrust curve
Propulsive efficiency η_prop vs flight speed. Pusher vs tractor comparison. Thermal efficiency of Rotax 915 iS and TPE331-10. Overall efficiency chain. Thrust available curve vs speed.
MODULE 12
Cruise Speed & Fuel Burn
DELTA · TIER 3+
- V_cruise
- SFC
- fuel/km
- endurance
Cruise speed optimisation at target altitude. Specific fuel consumption (SFC) for each engine option. Fuel burn per km and per hour at cruise and loiter conditions. Range sensitivity.
MODULE 13
Centre of Gravity Range
SIGMA · TIER 4
- CG_fwd
- CG_aft
- %MAC
- loading chart
Forward and aft CG limits as % MAC. CG excursion during fuel burn and payload loading. CG loading chart for mission planning. Lateral CG balance for both platform configurations.
MODULE 14
Tail Volume Coefficient
SIGMA · TIER 4
- Vh (H-tail)
- Vv (V-tail)
- ruddevator
- moment arm
Horizontal and vertical tail volume coefficients. Conventional tail (UAV-LRS-2000) vs inverted-V ruddevator (UAV-PSH-001) comparative analysis. Sizing methodology and accepted ranges.
MODULE 15
Static Margin
SIGMA · TIER 4
- NP location
- SM (%MAC)
- pitch stiffness
- stability grade
Neutral point estimation using aerodynamic centre contributions. Static margin as % MAC for both platforms. Stability gradient Cmα. Acceptable static margin bands for UAV autopilot operation.
MODULE 16
PID Tuning Parameters
SIGMA · TIER 4
- Kp / Ki / Kd
- roll loop
- pitch loop
- yaw loop
Initial PID gain estimates for roll, pitch, and yaw loops based on aircraft dynamics. Inner-outer loop structure. Gain scheduling approach for altitude. Starting values for HIL/SIL simulation.
MODULE 17
Control Loop Architecture
SIGMA · TIER 4
- inner loop
- outer loop
- state machine
- modes
Full flight control system block diagram. Inner attitude loop, outer navigation loop, altitude and airspeed hold. Auto-takeoff, waypoint following, loiter, return-to-base, emergency modes.
MODULE 18
Redundancy Logic
SIGMA · TIER 4
- dual FCC
- sensor voting
- failsafe tree
- watchdog
Dual-channel FCC crosscheck logic. Sensor voting (3-out-of-3, 2-out-of-3). Failure detection and isolation (FDI) architecture. Failsafe decision tree: RTB, loiter, controlled descent. Watchdog timer logic.