Typhon
TYPHONTechnology Transition
Open Calls/TYP-2026-007
TYP-2026-007Active

Alternative Position, Navigation, and Timing (Alt-PNT) for GPS-Denied Environments

Typhon

Posted

Mar 9, 2026

Deadline

Sep 30, 2026

178

Days

:

19

Hours

Alt-PNTGPS-Denied OperationsInertial NavigationQuantum SensingTiming HoldoverSignals of OpportunityElectronic Warfare ResilienceAssured PNTMEMS IMUChip-Scale Atomic ClocksCelestial NavigationMulti-Domain Operations

Description

Typhon seeks innovative Alternative Position, Navigation, and Timing (Alt-PNT) solutions capable of sustaining military operations when GPS is degraded, denied, or spoofed. This Open Call accepts submissions on a rolling basis with quarterly review cycles. Offerors may propose solutions addressing one or more PNT modalities across any form factor — from chip-scale implementations for guided munitions to rack-mount systems for surface combatants and submarines.

Overall Objective

Identify, evaluate, and accelerate fielding of alternative PNT technologies that provide operationally relevant position accuracy and timing precision when GPS is unavailable, degraded, or contested. The objective encompasses solutions across the full spectrum of military platforms — dismounted soldiers, ground vehicles, unmanned aerial systems (UAS), guided munitions, rotary- and fixed-wing aircraft, surface combatants, and submarines — with the goal of establishing a layered, resilient PNT architecture that no single adversary capability can defeat.

Problem Statement

GPS dependence represents the single greatest cross-cutting vulnerability in the Department of War's operational architecture. Virtually every weapons system, platform, command-and-control network, and logistics function relies on GPS-derived position and timing signals. The constellation's signal strength at Earth's surface (approximately -130 dBm) makes it inherently vulnerable to both jamming and spoofing. Peer adversaries — principally China and Russia — have demonstrated sophisticated electronic warfare capabilities that can deny GPS over areas exceeding 300 kilometers in radius.

Desired Solution

Offerors shall propose Alt-PNT solutions in one or more of the following technology areas: (1) advanced inertial navigation systems (INS) including MEMS, fiber-optic gyroscope (FOG), ring laser gyroscope (RLG), and cold-atom/quantum inertial measurement units (IMU); (2) signals of opportunity (SoOp) exploitation including LEO satellite constellations, cellular, digital television, FM/AM broadcast, and other ambient RF sources; (3) non-RF navigation including magnetic anomaly navigation (MAGNAV), gravity gradiometry, terrain-referenced navigation, visual-inertial odometry, and celestial navigation; (4) precision timing sources including chip-scale atomic clocks (CSAC), miniature rubidium standards, optical atomic clocks, and timing distribution architectures; and (5) multi-source PNT fusion engines that integrate two or more modalities.

Key Attributes

Position & Navigation Accuracy

Dismounted Horizontal CEP (60 min GPS-denied)Threshold: ≤25 meters; Objective: ≤10 meters
Vehicle/UAS Horizontal CEP (120 min GPS-denied)Threshold: ≤20 meters; Objective: ≤5 meters
Munition Terminal CEP (300 sec flight)Threshold: ≤10 meters; Objective: ≤3 meters
Platform CEP (24 hr GPS-denied)Threshold: ≤100 meters; Objective: ≤50 meters

Timing & Synchronization

UTC Holdover (1 hour, no GPS)Threshold: ≤1 microsecond; Objective: ≤100 nanoseconds
Extended Holdover (24 hours, platform-class)Threshold: ≤100 microseconds; Objective: ≤10 microseconds
Munition Timing (600 sec mission)Threshold: ≤10 microseconds; Objective: ≤1 microsecond
1PPS Output AccuracyThreshold: ≤500 nanoseconds to UTC; Objective: ≤50 nanoseconds to UTC

SWaP-C by Form Factor

Chip-Scale (munition-class)Requirement: ≤10 cm³, ≤50 g, ≤1 W, ≤$500/unit at 10K qty
Soldier-PortableRequirement: ≤200 cm³, ≤500 g, ≤5 W including antenna/sensor
Vehicle/UAS ModuleRequirement: ≤2,000 cm³, ≤5 kg, ≤25 W
Platform Rack-MountRequirement: ≤1/2 ATR, ≤15 kg, ≤100 W

Environmental & Robustness

Operating Temperature (ground)Requirement: -40°C to +71°C per MIL-STD-810H
Operating Temperature (munition)Requirement: -54°C to +85°C per MIL-STD-810H
Shock (munition-class)Requirement: Survive ≥20,000 g setback per MIL-STD-810H
VibrationRequirement: Per MIL-STD-810H Method 514.8, Category 4 minimum

Submission Scoring Rubric

Technical Merit & Innovation

35%
PNT Accuracy
Demonstrated PNT accuracy relative to threshold/objective requirements, supported by test data or validated simulation
Novelty
Technical novelty and differentiation from existing fielded or programmed solutions
Robustness
Robustness of approach to diverse GPS-denial scenarios including wideband jamming, spoofing, and indoor/underground/urban canyon environments

Technology Maturity & Fieldability

25%
Current TRL
Current Technology Readiness Level with credible evidence — hardware demonstrations, test reports
TRL Advancement
Realistic plan to advance from current TRL to TRL 7 within 24 months
Manufacturing Readiness
Path to production quantities at stated SWaP-C targets

SWaP-C & Scalability

20%
SWaP-C Compliance
Compliance with SWaP-C targets for proposed form factor(s)
Unit Cost
Credible unit cost projections at production quantities (1K, 10K, 100K units)
Scalability
Scalability across multiple form factors or platform classes from a common technology base

Integration & Operational Utility

20%
Compatibility
Compatibility with existing DoW PNT architectures, interfaces, and standards
Integration Burden
Minimal integration burden on host platform — low SWaP overhead, standard interfaces
Operational Concept
Operational concept addressing realistic military scenarios including rapid deployment and field calibration

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