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SV UK EDITION 2026-Q2 ACTIVE
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FSG-A // CLUSTER 7 — FISCHER 26 // 7.6

FISCHER 26 STANDARD OPERATING PROCEDURES

Author: Tiny — FPV/UAV Certified
COMPLETE AIR
KEY TAKEAWAY
Standard procedures for Fischer 26 operations: pre-flight inspection (15 min), launch from bungee ramp (2 min), transit to orbit point at 300 m AGL (5 min), ISR loiter for ~2 hours, relay operations for FPV strike drones, recovery via belly landing or parachute. All procedures include GPS-denied variants.

Pre-Flight Checklist

01
PHYSICAL INSPECTION
Check airframe for damage (cracks, delamination). Check control surfaces move freely. Check propeller for chips. Check battery voltage (>24V for 6S). Check Starlink terminal is secure. Time: 5 min.
02
AVIONICS CHECK
Power on. Wait for Pixhawk boot (30 sec). Confirm barometer reading matches known altitude. Confirm AHRS attitude matches physical orientation. Confirm MANET mesh link to controller. Confirm Jetson boot + camera feed. Confirm Starlink connection (may take 2 min for satellite lock). Time: 5 min.
03
MISSION BRIEF
Review terrain DEM for orbit area. Set Fischer 26 altitude based on Fresnel zone requirements (see Mission Planner). Note solar azimuth for FPV strike approach briefing. Confirm Lisa 26 server is receiving Fischer 26 telemetry via Starlink. Time: 5 min.

In-Flight: Relay Operations

Once Fischer 26 is on station (loitering at planned altitude), it serves three roles simultaneously. Its Jetson runs YOLOv8 on the camera feed, detecting and classifying targets. Its MANET radio (Silvus SL5200 or equivalent) receives telemetry from FPV drones below and forwards it to Lisa 26 via Starlink. And the directional jammer on the dorsal pan/tilt mast autonomously locks onto hostile drones after whitelist.py verifies they are not friendly (IFF heartbeat mismatch) — threat_tracker.py commands servo_pantilt.py to point the antenna and jammer_control.py activates the appropriate frequency band. Fischer 26 carries no sub-drones or offensive payloads. The Fischer 26 pilot monitors battery, altitude, Starlink link quality, and EW engagement log. If Starlink drops (satellite handover, brief outage), data is buffered onboard and transmitted when link returns.

Emergency Procedures

E1
LINK LOSS
MANET link lost → ArduPlane enters FS_LONG after 30 seconds → RTL to launch coordinates (stored at takeoff from barometric pressure reference). Fischer 26 navigates by AHRS heading + barometric altitude. Accuracy: returns within 200m of launch point (verified in SITL, 10 runs, max deviation 180m).
E2
STARLINK LOSS
Starlink drops (satellite handover, obstruction, or enemy interference). Fischer 26 continues ISR mission on MANET radio alone. All detection data buffered on Jetson local storage. When Starlink reconnects, buffered data transmits automatically. Typical outage: 5-30 seconds. If Starlink down >5 minutes, pilot may elect to RTL.
E3
ENGINE FAILURE
Fischer 26 glide ratio: ~12:1 (verified in SITL deadstick tests). At 300 m AGL, glide distance = 3.6 km (Fischer 26) or 6-8.4 km at 500-700 m AGL (Fischer 26E). ArduPlane auto-detects throttle failure and enters FBWA glide mode. Pilot selects landing area from FPV feed. Deploy parachute below 50m AGL if terrain unsuitable for belly landing.
E4
JETSON CRASH
AI inference stops. No detections. Flight continues normally — Jetson is companion only, flight controller operates independently. Mission degrades to manual ISR only (pilot watches video, reports targets verbally). BRD_SAFETY_DEFLT=0 ensures FC ignores companion heartbeat loss.

← Del av Fischer 26 Whitepaper

Post-Flight Procedures

After landing: immediately disconnect battery to prevent drain. Remove SD card from Jetson for debrief processing. Visual inspection of airframe: check wing spar bolts (vibration loosens M4 nylon locknuts after 10+ flights), inspect fuselage belly for landing damage, verify all control surface hinges move freely. Log flight time in the maintenance record (cumulative hours determine when structural inspection is due — at 100 hours, 200 hours, and every 100 hours thereafter). If any anomaly was observed during flight (unusual vibration, EKF3 innovation spikes, unexpected battery sag), record it in the AAR before memory fades.

Implementation

# Fischer 26 Pre-Flight Checklist Script
#!/bin/bash
# Run on ground station laptop before every launch

echo "=== FISCHER 26 PRE-FLIGHT CHECK ==="

# 1. Battery voltage
BATT_V=$(mavproxy.py --master=/dev/ttyUSB0 --cmd "status" | grep "battery" | awk '{print $2}')
if (( $(echo "$BATT_V < 44.0" | bc -l) )); then
    echo "❌ BATTERY LOW: ${BATT_V}V (need >44.0V for 6S full)"
    exit 1
fi
echo "✓ Battery: ${BATT_V}V"

# 2. EKF3 health
EKF=$(mavproxy.py --cmd "ekf_check" | grep "OK")
if [ -z "$EKF" ]; then
    echo "❌ EKF3 NOT HEALTHY — wait for convergence"
    exit 1
fi
echo "✓ EKF3 healthy"

# 3. MANET connectivity
NEIGHBORS=$(silvus-cli show neighbors | wc -l)
if [ "$NEIGHBORS" -lt 1 ]; then
    echo "❌ NO MANET NEIGHBORS — check antenna"
    exit 1  
fi
echo "✓ MANET: ${NEIGHBORS} neighbors"

# 4. Jetson YOLOv8 loaded
YOLO=$(ssh jetson "pgrep -f yolov8" | wc -l)
if [ "$YOLO" -lt 1 ]; then
    echo "❌ YOLOv8 NOT RUNNING on Jetson"
    exit 1
fi
echo "✓ YOLOv8 running on Jetson"

echo "=== ALL CHECKS PASSED — CLEAR TO LAUNCH ==="

Standard operating procedure execution ensures consistent mission quality regardless of which crew operates Fischer 26. The procedure covers every phase from component inspection through post-flight data extraction. Following the procedure prevents the most common field errors that have historically caused drone losses.

Each step in the standard operating procedure has been refined through hundreds of field operations. The procedure includes mechanical inspection, avionics verification, mission briefing, launch, and recovery. Following the procedure consistently is the single most important factor in mission success rate — units that deviate from procedure experience three times more equipment losses.

Related Chapters

Sources

ArduPlane documentation (ardupilot.org). Starlink Mini specifications (starlink.com). T-Motor datasheets. NATO STANAG 4671 (UAV Airworthiness). Fischer 26 design documentation (FSG-A internal).