Parameter Identification of a Surface-to-Surface Missile\ud from Flight Test Data

Specification of flight test maneuvers for identification\ud experiments on a Jaguar aircraft

Parameswaran, V
Girija, G
Raol, JR

January 1985

This document presents the specifications of flight test maneuvers for estimation of Lift and Drag c...

Aerodynamic Parameter Estimation for Prithvi from first Flight Test Data:Preliminary Result 2

Shantha Kumar, N

February 1990

This document represents Preliminary investigations made to evaluate aerodynamic model for Prithvi m...

Missile Datcom, user's manual -- revision 6/93 /

Burns, Keith A., author.
Blake, William B., author.
Vukelich, Steven R., author.
Stoy, Stan L., author.
Deters, Kenneth J., author.
Wright Laboratory (Wright-Patterson Air Force Base, Ohio), sponsor.
McDonnell Douglas Astronautics Company-St. Louis, sponsor.

In missile preliminary design it is necessary to quickly and economically estimate the aerodynamics ...

Post Flight Missile Parameter Identification for aeroballistic range

Mohan Ram, VS
Srinatha Sastry, CV

October 1985

This document is a detailed project proposal for estimation\ud of aerodynamic parameters of missile ...

Aerodynamic Parameter Estimation For Prithvi From First Flight Test Data Preliminary Results 2\ud

Shantha Kumar, N
Raol, JR
Balakrishna, S

February 1990

This Document Presents Preliminary Investigations Made To Evaluate Aerodynamic Model For Prithvi Mis...

Estimation of Aerodynamic Derivatives of Missiles from Range and Simulated Data Using Nonlinear Maximum Likelihood Method.

Raol, JR
Girija, G
Mohan Ram, VS

January 1988

This document contains the results of estimation of aerodynamic derivatives of (i) the AGARD standar...

Analysis and compilation of missile aerodynamic data.

Nichols, James O.
Auburn University. Dept. of Aerospace Engineering.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1977

This summary document was prepared in order to facilitate dissemination of a large amount of missile...

Missile aerodynamic parameter and structure identification from flight test data /

Kain, James E., author
Lee, Jang G., author.
Brown, Charles M., Jr., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.
Analytic Sciences Corporation. sponsor.

"Final Report for the period February 1977 to October 1977.""November 1977."Includes bibliographical...

Estimation of Aerodynamic Derivatives of Missiles from Range\ud and Simulated Data Using Nonlinear Maximum Likelihood Method.

Raol, JR
Girija, G
Mohan Ram, VS

January 1988

This document contains the results of estimation of aerodynamic derivatives of (i) the AGARD standar...

Aerodynamic Force Measurement On A 1/10th Scale Model Of AGNI Missile Payload Plus IInd Stage.\ud

Vinay Kumar, -

August 1990

Wind Tunnel Tests Were Carried Out To Determine The Aerodynamic Characteristics Of A 1/10th Scale Pa...

Specifications Of Test Maneuvers For Generating Flight Data For Parameter Estimation And Simulation Of Unconventional Aircraft

Padma, Madhuranath
Parameswaran, V
Raol, JR

February 1991

This Document Contains Flight Test Matrices And Describes Various Flight Test Maneuvers To Generate...

Missile Aerodynamics Design Manual

Anon, -

November 1987

This proposal describes the first phase of the work comtemplated for the Missile Design Manual . The...

Specifications Of Test Maneuvers For Generating Flight Data For Parameter Estimation And Simulation Of Unconventional Aircraft\ud

Padma, Madhuranath
Parameswaran, V
Raol, JR

February 1991

This Document Contains Flight Test Matrices And Describes\ud Various Flight Test Maneuvers To Genera...

Experimental studies on a 1/10th scale model of Agni- payload missile

Vinay Kumar, -

March 1989

Wind tunnel tests were carried out to determine the aerodynamic characteristics of a 1/10th scale AG...

Aerodynamic test and analysis of a slender generic missile configuration /

Gates, Roger S., author
Fische, Mark A., author.
Cipolla, John R., author.
Winchenback, G. L., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Program Element No. 62602F, Project No. 2567, Task No, 03, Work Unit Accession No. 12.""Interim Rep...

Specification of flight test maneuvers for identification\ud experiments on a Jaguar aircraft

Parameswaran, V
Girija, G
Raol, JR

January 1985

This document presents the specifications of flight test maneuvers for estimation of Lift and Drag c...

Aerodynamic Parameter Estimation for Prithvi from first Flight Test Data:Preliminary Result 2

Shantha Kumar, N

February 1990

This document represents Preliminary investigations made to evaluate aerodynamic model for Prithvi m...

Missile Datcom, user's manual -- revision 6/93 /

Burns, Keith A., author.
Blake, William B., author.
Vukelich, Steven R., author.
Stoy, Stan L., author.
Deters, Kenneth J., author.
Wright Laboratory (Wright-Patterson Air Force Base, Ohio), sponsor.
McDonnell Douglas Astronautics Company-St. Louis, sponsor.

In missile preliminary design it is necessary to quickly and economically estimate the aerodynamics ...

Post Flight Missile Parameter Identification for aeroballistic range

Mohan Ram, VS
Srinatha Sastry, CV

October 1985

This document is a detailed project proposal for estimation\ud of aerodynamic parameters of missile ...

Aerodynamic Parameter Estimation For Prithvi From First Flight Test Data Preliminary Results 2\ud

Shantha Kumar, N
Raol, JR
Balakrishna, S

February 1990

This Document Presents Preliminary Investigations Made To Evaluate Aerodynamic Model For Prithvi Mis...

Estimation of Aerodynamic Derivatives of Missiles from Range and Simulated Data Using Nonlinear Maximum Likelihood Method.

Raol, JR
Girija, G
Mohan Ram, VS

January 1988

This document contains the results of estimation of aerodynamic derivatives of (i) the AGARD standar...

Analysis and compilation of missile aerodynamic data.

Nichols, James O.
Auburn University. Dept. of Aerospace Engineering.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1977

This summary document was prepared in order to facilitate dissemination of a large amount of missile...

Missile aerodynamic parameter and structure identification from flight test data /

Kain, James E., author
Lee, Jang G., author.
Brown, Charles M., Jr., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.
Analytic Sciences Corporation. sponsor.

"Final Report for the period February 1977 to October 1977.""November 1977."Includes bibliographical...

Estimation of Aerodynamic Derivatives of Missiles from Range\ud and Simulated Data Using Nonlinear Maximum Likelihood Method.

Raol, JR
Girija, G
Mohan Ram, VS

January 1988

This document contains the results of estimation of aerodynamic derivatives of (i) the AGARD standar...

Aerodynamic Force Measurement On A 1/10th Scale Model Of AGNI Missile Payload Plus IInd Stage.\ud

Vinay Kumar, -

August 1990

Wind Tunnel Tests Were Carried Out To Determine The Aerodynamic Characteristics Of A 1/10th Scale Pa...

Specifications Of Test Maneuvers For Generating Flight Data For Parameter Estimation And Simulation Of Unconventional Aircraft

Padma, Madhuranath
Parameswaran, V
Raol, JR

February 1991

This Document Contains Flight Test Matrices And Describes Various Flight Test Maneuvers To Generate...

Missile Aerodynamics Design Manual

Anon, -

November 1987

This proposal describes the first phase of the work comtemplated for the Missile Design Manual . The...

Specifications Of Test Maneuvers For Generating Flight Data For Parameter Estimation And Simulation Of Unconventional Aircraft\ud

Padma, Madhuranath
Parameswaran, V
Raol, JR

February 1991

This Document Contains Flight Test Matrices And Describes\ud Various Flight Test Maneuvers To Genera...

Experimental studies on a 1/10th scale model of Agni- payload missile

Vinay Kumar, -

March 1989

Wind tunnel tests were carried out to determine the aerodynamic characteristics of a 1/10th scale AG...

Aerodynamic test and analysis of a slender generic missile configuration /

Gates, Roger S., author
Fische, Mark A., author.
Cipolla, John R., author.
Winchenback, G. L., author.
United States. Air Force. Systems Command. sponsor.
Air Force Armament Laboratory. issuing body.

"Program Element No. 62602F, Project No. 2567, Task No, 03, Work Unit Accession No. 12.""Interim Rep...

Specification of flight test maneuvers for identification\ud experiments on a Jaguar aircraft

Parameswaran, V
Girija, G
Raol, JR

January 1985

This document presents the specifications of flight test maneuvers for estimation of Lift and Drag c...

Aerodynamic Parameter Estimation for Prithvi from first Flight Test Data:Preliminary Result 2

Shantha Kumar, N

February 1990

This document represents Preliminary investigations made to evaluate aerodynamic model for Prithvi m...

Missile Datcom, user's manual -- revision 6/93 /

Burns, Keith A., author.
Blake, William B., author.
Vukelich, Steven R., author.
Stoy, Stan L., author.
Deters, Kenneth J., author.
Wright Laboratory (Wright-Patterson Air Force Base, Ohio), sponsor.
McDonnell Douglas Astronautics Company-St. Louis, sponsor.

In missile preliminary design it is necessary to quickly and economically estimate the aerodynamics ...

Parameter Identification of a Surface-to-Surface Missile\ud from Flight Test Data

Abstract

Extracted data

Parameter Identification of a Surface-to-Surface Missile\ud from Flight Test Data

Abstract

Extracted data

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