SE9801736L - Method of simulating a real robot by means of a robot simulator when testing an aircraft system comprising a weapon system - Google Patents

Method of simulating a real robot by means of a robot simulator when testing an aircraft system comprising a weapon system

Info

Publication number
SE9801736L
SE9801736L SE9801736A SE9801736A SE9801736L SE 9801736 L SE9801736 L SE 9801736L SE 9801736 A SE9801736 A SE 9801736A SE 9801736 A SE9801736 A SE 9801736A SE 9801736 L SE9801736 L SE 9801736L
Authority
SE
Sweden
Prior art keywords
missile
robot
weapons system
simulating
testing
Prior art date
Application number
SE9801736A
Other languages
Unknown language ( )
Swedish (sv)
Other versions
SE513330C2 (en
SE9801736D0 (en
Inventor
Lars-Olof Oehberg
Bernt-Ove Hedman
Original Assignee
Saab Ab
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Saab Ab filed Critical Saab Ab
Priority to SE9801736A priority Critical patent/SE513330C2/en
Publication of SE9801736D0 publication Critical patent/SE9801736D0/en
Priority to EP99927033A priority patent/EP1078214B1/en
Priority to PCT/SE1999/000751 priority patent/WO1999060326A1/en
Priority to ES99927033T priority patent/ES2214858T3/en
Priority to AT99927033T priority patent/ATE258674T1/en
Priority to DE69914474T priority patent/DE69914474T2/en
Publication of SE9801736L publication Critical patent/SE9801736L/en
Publication of SE513330C2 publication Critical patent/SE513330C2/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/006Guided missiles training or simulation devices

Abstract

A method for simulating an actual missile, by means of a missile simulator, aircraft system which comprises a weapons system (1), where the missile is controlled from the weapons system (1) by a error signal (6) in a control loop by means of the said error signal (6) positioning a target seeker in the missile and through the sending back of the target seeker's position to the weapons system via an actual value signal (8), where a) the target seeker in the missile is commanded by the weapons system (1) to adopt a predetermined position, b) the missile simulator measures the control loop's error signal (6), generates an actual value for the position of the target seeker and sends the actual value (8) to the weapons system (1), c) the weapons system (1) calculates a new error signal (6) for the control loop and where d) steps b to c are repeated during the test. By using the method, an actual missile is not needed during the testing.
SE9801736A 1998-05-15 1998-05-15 Method of simulating a real robot by means of a robot simulator when testing an aircraft system comprising a weapon system SE513330C2 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
SE9801736A SE513330C2 (en) 1998-05-15 1998-05-15 Method of simulating a real robot by means of a robot simulator when testing an aircraft system comprising a weapon system
EP99927033A EP1078214B1 (en) 1998-05-15 1999-05-05 Missile simulator
PCT/SE1999/000751 WO1999060326A1 (en) 1998-05-15 1999-05-05 Robot simulator
ES99927033T ES2214858T3 (en) 1998-05-15 1999-05-05 MISSILE SIMULATOR.
AT99927033T ATE258674T1 (en) 1998-05-15 1999-05-05 MISSILE SIMULATOR
DE69914474T DE69914474T2 (en) 1998-05-15 1999-05-05 MISSILE SIMULATOR

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE9801736A SE513330C2 (en) 1998-05-15 1998-05-15 Method of simulating a real robot by means of a robot simulator when testing an aircraft system comprising a weapon system

Publications (3)

Publication Number Publication Date
SE9801736D0 SE9801736D0 (en) 1998-05-15
SE9801736L true SE9801736L (en) 1999-11-16
SE513330C2 SE513330C2 (en) 2000-08-28

Family

ID=20411349

Family Applications (1)

Application Number Title Priority Date Filing Date
SE9801736A SE513330C2 (en) 1998-05-15 1998-05-15 Method of simulating a real robot by means of a robot simulator when testing an aircraft system comprising a weapon system

Country Status (6)

Country Link
EP (1) EP1078214B1 (en)
AT (1) ATE258674T1 (en)
DE (1) DE69914474T2 (en)
ES (1) ES2214858T3 (en)
SE (1) SE513330C2 (en)
WO (1) WO1999060326A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005058546A1 (en) * 2005-12-08 2007-06-14 Lfk-Lenkflugkörpersysteme Gmbh A weapons station testing unit and method of testing the operational readiness of a weapon station of an aircraft
US8046203B2 (en) * 2008-07-11 2011-10-25 Honeywell International Inc. Method and apparatus for analysis of errors, accuracy, and precision of guns and direct and indirect fire control mechanisms
CN110849214B (en) * 2019-11-29 2022-03-04 北京仿真中心 Sight line correction method for offset installation of target simulator and optical seeker on five-axis turntable

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0309133A2 (en) * 1987-09-11 1989-03-29 British Aerospace Public Limited Company Digital weapon simulator
CA2100156C (en) * 1992-07-13 1998-07-28 Ronald W. Monk Method and apparatus for missile interface testing
US5415548A (en) * 1993-02-18 1995-05-16 Westinghouse Electric Corp. System and method for simulating targets for testing missiles and other target driven devices
US5721680A (en) * 1995-06-07 1998-02-24 Hughes Missile Systems Company Missile test method for testing the operability of a missile from a launch site

Also Published As

Publication number Publication date
DE69914474D1 (en) 2004-03-04
SE513330C2 (en) 2000-08-28
EP1078214B1 (en) 2004-01-28
EP1078214A1 (en) 2001-02-28
SE9801736D0 (en) 1998-05-15
WO1999060326A1 (en) 1999-11-25
DE69914474T2 (en) 2004-11-11
ATE258674T1 (en) 2004-02-15
ES2214858T3 (en) 2004-09-16

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