Objectives 1-6 Flashcards
List the capabilities of 4th and 5th generation aircraft
4th Generation (1980-2000): Multimode pulse-doppler radar, DRFM jammers, active AAM, high-off boresight IR missiles
5th Generation (2000- ): AESA radar, integrated defensive avionics, long-wave IRSTS, thrust vector capability, weapons with cooperative engagement capability
Describe the FSU models of radar control of fighters
FSU: Close Control
See Slide 15 for definition
ID the key information from a launch acceptability region table
Define:
Rkin
F-pole
IR LAR key term
See slides 24 and 25 for examples of a LAR
Key terms:
Rkin - Missiles raw, kinematic range. Not limited by fire control or seeker acquisition capabilities.
F-pole - range between launcher and target at time of semiactive missile endgame/impact
See slide 25 for IR LAR key term
Describe and/or illustrate the missile guidance schemes used by radar SAM systems: Active Guidance
A FC sensor establishes a track on a target, either with an EO/IR tracker or with a TTR. During the engagement A SEEKER ONBOARD THE MISSILE tracks the target.
-Still must use ground radar
Describe radar SAM acquisition radar purpose and configuration
Purpose: to find the target aircraft using pointing data from C2 and IADS
Configuration: Offboard acquisition radars: - Physically separated from TTR - Target Info passed via data link, cable, and voice - Local sensors allow for decentralized control Onboard acquisition radars: - Radars on same vehicle as TTR - Allows autonomous operations
Describe and/or illustrate the missile guidance schemes used by radar SAM systems: SAR homing** guidance
A FC sensor establishes a track on a target, either with an EO/IR tracker or with a TTR. When ready to fire, the target illuminator paints the target, typically with a CW illuminator. The SAR MISSILE HOMES IN ON THE ENERGY REFLECTED OFF THE TARGET.
Describe and/or illustrate the missile guidance schemes used by radar SAM systems: Command Guidance
Command-guided missiles are steered to the target by commands transmitted from the ground-based FC system. The ground TTR tracks both the target and the missile. THE GROUND RADAR PROVIDES THE MISSILE STEERING COMMANDS.
Describe and/or illustrate the missile guidance schemes used by radar SAM systems: Combined Guidance Schemes
Track via missile:
Combines Command and SAR guidance
Inertial Guidance:
Combines Command guidance and INS hardware
For a LAR diagram, define:
Rmax1
Rmax2
Rmax1 - Maximum displayed missile employment range and the missiles maximum FC launch permit range (sometimes Rmax)
Rmax2 - Refers to heart of envelope shot that accounts for some evasive maneuvers by the target at endgame
Describe Command to Line of Sight guidance law
Most inefficient guidance law. Think pure pursuit.
For crossing aircraft: missile drifts aft on canopy
For inbound/outbound aircraft: straighter flight path with less drift
Describe half-rectified guidance law
Missile is guided to a point halfwat between the target position and predicted intercept point.
Poor mans pro-nav.
For a crossing target: missile drifts aft slowly on canopy.
ID crossrange info when given a SAM engagement envelope diagram
See slides 63-66
Describe Proportional Navigation
MOST EFFICIENT TRAJECTORY.
Missile appears steady on canopt to a nonmanuevering target aircraft.
IR SAMS, MANPADS, SARH and advanced command guided SAMS.