Skip to main content
Glama

density_altitude_calculator

Calculate density altitude from pressure altitude and temperature for accurate aircraft performance assessment.

Instructions

Calculate density altitude from pressure altitude and temperature.

Density altitude is the altitude in the standard atmosphere at which the air density equals the actual air density at the given conditions. Essential for aircraft performance calculations.

Args: pressure_altitude_ft: Pressure altitude in feet temperature_c: Outside air temperature in Celsius dewpoint_c: Optional dewpoint for humidity correction

Returns: Formatted string with density altitude calculation results including air density, density ratio (sigma), pressure ratio (delta), and ISA deviation.

Raises: No exceptions are raised directly; errors are returned as formatted strings.

Input Schema

TableJSON Schema
NameRequiredDescriptionDefault
pressure_altitude_ftYes
temperature_cYes
dewpoint_cNo

Output Schema

TableJSON Schema
NameRequiredDescriptionDefault
resultYes
Behavior4/5

Does the description disclose side effects, auth requirements, rate limits, or destructive behavior?

No annotations provided, so description bears full burden. Describes inputs, output format (formatted string), and error handling (errors returned as strings). Missing side effects or computational limits.

Agents need to know what a tool does to the world before calling it. Descriptions should go beyond structured annotations to explain consequences.

Conciseness4/5

Is the description appropriately sized, front-loaded, and free of redundancy?

Well-structured with a brief opening, definition, and docstring-style Args/Returns/Raises. Front-loaded with core purpose, though Returns section is slightly verbose.

Shorter descriptions cost fewer tokens and are easier for agents to parse. Every sentence should earn its place.

Completeness4/5

Given the tool's complexity, does the description cover enough for an agent to succeed on first attempt?

Covers purpose, parameters, output (formatted string with specific values), and error handling. Output schema exists, so return values are partly defined. Lacks output units and validity ranges.

Complex tools with many parameters or behaviors need more documentation. Simple tools need less. This dimension scales expectations accordingly.

Parameters5/5

Does the description clarify parameter syntax, constraints, interactions, or defaults beyond what the schema provides?

Schema description coverage is 0%, but description adds units and meaning for all three parameters: pressure_altitude_ft in feet, temperature_c in Celsius, dewpoint_c optional for humidity correction. Goes well beyond schema.

Input schemas describe structure but not intent. Descriptions should explain non-obvious parameter relationships and valid value ranges.

Purpose5/5

Does the description clearly state what the tool does and how it differs from similar tools?

Clearly states the tool calculates density altitude from pressure altitude and temperature, with a definition and significance. Distinct from siblings like stall_speed_calculator.

Agents choose between tools based on descriptions. A clear purpose with a specific verb and resource helps agents select the right tool.

Usage Guidelines3/5

Does the description explain when to use this tool, when not to, or what alternatives exist?

Mentions essential for aircraft performance calculations but does not specify when to use vs alternatives or exclusion conditions. No guidance on when not to use.

Agents often have multiple tools that could apply. Explicit usage guidance like "use X instead of Y when Z" prevents misuse.

Install Server

Other Tools

Latest Blog Posts

MCP directory API

We provide all the information about MCP servers via our MCP API.

curl -X GET 'https://glama.ai/api/mcp/v1/servers/cheesejaguar/aerospace-mcp'

If you have feedback or need assistance with the MCP directory API, please join our Discord server